Loading...
Welcome to Acta Armamentarii ! Today is

Table of Content

    28 April 2023, Volume 44 Issue 4
    Electronic edition of this issue
    Electronic edition of this issue
    2023, 44(4):  0. 
    Asbtract ( )   PDF (173085KB) ( )  
    Related Articles | Metrics
    Contents
    Contents
    2023, 44(4):  0. 
    Asbtract ( )   PDF (1025KB) ( )  
    Related Articles | Metrics
    Assessment and Experimental Study of Damage Power of Anti-Submarine Warhead to the Pressure Hull Structure
    WANG Shushan, GUI Qiuyang, LU Xi, JIA Xiyu, GAO Yuan, LIANG Ce
    2023, 44(4):  919-928.  doi:10.12382/bgxb.2021.0871
    Asbtract ( )   HTML ( )   PDF (5514KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    Considering the characteristics of different anti-submarine (torpedo/depth charge) warheads, including multiple effects of underwater explosions, and multiple styles of target structures, the normalized comprehensive damage power characterization and assessment of warheads were studied. Based on the damage of the most representative hull structure (pressure hull) and comprehensively considering the effects of large deformation, tearing, and perforation, a method to quantitatively characterize and evaluate the power of the warhead through a comprehensive damage power index was proposed. A test target simulating the damaging effect of single-hull, and the double-hull was designed, and three model warheads were tested. The comprehensive power of the three warheads against the two types of structures was obtained. The results showed that: the proposed comprehensive power assessment method has scientific rationality and engineering practicability; it can quantitatively compare and analyze the differences in the damage power of the same warhead to different hull structures and the damage power of different warheads to the same hull structure; under the same conditions, the blast warhead and the shaped charge warhead had relatively greater damage to the single-hull target and double-hulled targets; implosion warheads had better damage power to both types of targets; for different targets, the damage power of the blast warhead, the implosion warhead, and the implosion warhead dropped by more than 90%, nearly 80%, and less than 20%, respectively.

    Damage Effects and Engineering Computational Model of Internal Explosion of Airfield Runway
    HU Rong, JIANG Chunlan, LU Guangzhao, WANG Zaicheng, MAO Liang
    2023, 44(4):  929-939.  doi:10.12382/bgxb.2022.1220
    Asbtract ( )   HTML ( )   PDF (11822KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    To systematically investigate the damage effects of airfield runways subjected to charge implosion and construct an engineering function model, experiments and numerical simulations are conducted using dimension analytics to study the influence of charge quality and buried depth levels on damage modes and damage parameters of airfield runways. Results indicate that the effective damage radius (Red) initially increases and then decreases with an increase in buried depth of charge at a constant charge quantity. Conversely, damage parameters increase with an increasing charge quantity when the buried depth is constant, and an optimal matching of explosion energy and buried depth can achieve the ideal damage. Additionally, based on the analysis of the mechanism of implosion in the runways, an evaluation method which combines damage mode and damage parameters to effectively characterize the damage of implosion in airfield runways is proposed. Based on the crater pattern and cracks obtained from experiments and numerical simulations, there are three damage modes of the runways: open crater, heave crater, and camouflet. The crater radius Rc, effective damage radius Red, maximum internal cavity radius Ric, and actual crater depth H are used as characteristic parameters to quantitatively describe the damage within the runways. An engineering model to predict the damage mode and damage parameters of implosion on airfield runways is also constructed based on a large number of simulations and experimental data, achieving rapid prediction of airfield runway implosion damage effects.

    Vehicle Target Recognition Algorithm Based on MEMS LiDAR
    HUO Jian, CHEN Huimin, MA Yunfei, GUO Pengyu, YANG Xu, MENG Xiangsheng
    2023, 44(4):  940-948.  doi:10.12382/bgxb.2021.0822
    Asbtract ( )   HTML ( )   PDF (6643KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    In order to solve the problem of low recognition accuracy of traditional linear array Lidar, recognition algorithm based on MEMS LiDAR pushbroom scanning is designed. To reduce the amount of computation, directly filtering and grid segmentation algorithms are introduced to reduce the amount of original point clouds and effectively improve the real-time performance of detection. Combined with the organized processing method of MEMS LiDAR point cloud, a point cloud clustering algorithm based on mathematical morphology is proposed, which divides the point clouds after removing the ground points into independent point cloud clusters. The denoising algorithm based on distribution histogram with adaptive threshold is used to remove the outlier noise points around the targets. On this basis, a multifeature composite criterion is designed to directly process the three-dimensional LiDAR point clouds after clustering denoising to realize the accurate recognition of the targets. The data processing results under different experimental conditions are analyzed, and the recognition accuracy reaches 94.9%, which shows that the method has good generalization ability and accuracy.

    A Method for Specific Communication Emitter Identification Based on Multi-Domain Feature Fusion
    WANG Jian, ZHANG Bangning, ZHANG Jie, WEI Guofeng, GUO Daoxing
    2023, 44(4):  949-959.  doi:10.12382/bgxb.2021.0880
    Asbtract ( )   HTML ( )   PDF (5785KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    To solve the problem of low identification rate caused by specific communication emitter identification using a single feature, a method for individual identification of the communication emitter based on multi-domain feature fusion is proposed. Firstly, multiple transform domain features of the signals transmitted by the communication emitter are extracted, and these features are combined into multi-domain features.Secondly, the multi-channel convolution neural network is constructed, and the multi-channel convolution operation is carried out to extract the multi-domain features at a deep level. Finally, specificcommunication emitter classification is completed using the neural network classifier.Compared with the identification method based on a single feature, this method makes full use of the multi-domain features of the signals sent by the communication emitter and combines the powerful microscopic feature mining capability of the neural network to realize the effective individual identification of the communication emitter. Through the identification of 20 CC2530 devices under the conditions of low signal-to-noise ratio(SNR) and Rayleigh channel, the results show that the proposed method can significantly improve the identification accuracy and timeliness under a low SNR, and that the identification effect can still reach 91.01% under the condition of 0dB.

    Trajectory Tracking Control of Unmanned Tracked Vehicles Based on Adaptive Dual-Parameter Optimization
    LU Jiaxing, LIU Haiou, GUAN Haijie, LI Derun, CHEN Huiyan, LIU Longlong
    2023, 44(4):  960-971.  doi:10.12382/bgxb.2022.0009
    Asbtract ( )   HTML ( )   PDF (5793KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    To improve the poor adaptability of trajectory tracking controllers with fixed parameters, an optimized adaptive dual-parameter trajectory tracking algorithm for unmanned tracked vehicles based on the improved Particle Swarm Optimization (IPSO) and Multi-Layer Perceptron (MLP) algorithms is proposed. In the offline state, based on the collected actual vehicle data, the IPSO algorithm is used to construct the optimal parameter data set under different motion primitives, aiming for high accuracy, high stability, and low time cost of trajectory tracking. With the motion primitive type and vehicle speed as feature vectors, control time domain length and control time step length as labels, adaptive learning rate optimization algorithm is used to complete the training of the MLP neural network model. In the online state, according to the trajectory information and vehicle state feedback information provided by the planning layer, the MLP neural network outputs the predicted optimal control time domain length and control time step. These parameters are then input to the model predictive controller as dual parameters, enabling the adaptive trajectory tracking control. ROS-VREP co-simulation test and actual vehicle test based on a bilateral electric drive platform are carried out. Vehicle test results show that under various working conditions including large curvature steering, the proposed controller achieves a 30.5% reduction in average lateral error, a 17.2% decrease in average heading error, and a 7.8% reduction in average change rate of rotation angle, compared with the fixed-parameter trajectory tracking control method with the same calculation time cost. The results verify the feasibility and effectiveness of the new algorithm.

    Effects of Multimodal Warning and Cognitive Load on the Response of Armored Vehicle Occupants
    SUN Xiaodong, JIN Xiaoping, XIE Fang, SUN Houjie, ZHENG Sijuan
    2023, 44(4):  972-981.  doi:10.12382/bgxb.2022.0018
    Asbtract ( )   HTML ( )   PDF (2668KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    To explore the effects of multimodal warning on the response of armored vehicle occupants regarding the direction of enemy vehicles under different cognitive load levels, 20 adult males were recruited to take two-factor ergonomic experiments on the warning type and cognitive load level. The experiments were based on a virtual simulated armored vehicle occupant task platform designed for a hypothetical operational task for armored vehicle occupants and warned the occupants under different cognitive load levels about enemy vehicle directions. Results show that multimodal warning with haptics was easier for occupants to understand the situation and more in line with their cognitive state than visual warning. This type of warning significantly reduced their reaction time, annihilation time, and response error rate. Occupants with a high cognitive load level showed a significant decrease in information comprehension and a significant increase in reaction time, annihilation time, and response error rate compared to those with a lower load. The findings suggest that multimodal warning can be used to speed up occupant reaction and improve combat performance when the visual channel is overloaded or the cognitive load is high. This study provides a theoretical basis for designing multimodal human-computer interaction warnings in armored vehicle compartments.

    Oscillations Characteristics of One-dimensional Detonation Waves in Non-Uniform Hydrogen-Air Mixture
    XI Xuechen, YANG Pengfei, WANG Kuanliang
    2023, 44(4):  982-993.  doi:10.12382/bgxb.2021.0804
    Asbtract ( )   HTML ( )   PDF (4945KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    The inhomogeneity of the medium in front of the waves has a significant effect on the propagation of gaseous detonation waves, but the interaction mechanism remains unclear. The two-step induction-exothermic reaction model is used to study the propagation characteristics of one-dimensional hydrogen/air detonation waves in a non-uniform medium, and the influence of perturbation wavelength on detonation waves under different oscillation modes is analyzed. The results show that as the perturbation frequency get closer to the inherent oscillation frequency of detonation waves, the inherent instability is more easily triggered, resulting in more irregular oscillations. There are two dominant mechanisms of detonation waves propagating in a non-uniform medium. Pressure oscillation of weakly unstable detonation waves are dominated by density perturbation, and the main frequency of detonation pressure oscillation is consistent with the perturbation frequency; the pressure oscillation of strong detonation waves are dominated by inherent instability, and the oscillation frequency is distributed in the low frequency region without obvious dominant frequency, where perturbation only enhances the oscillation amplitude. When the perturbation is applied, the detonation waves under atmospheric pressure and at high altitudes has the above oscillation characteristics, which further confirms the feasibility of regulating detonation waves by artificial perturbation.

    Influence of Machining Parameters on the Milling Quality of T800 CFRP
    GAO Hang, LAN Baohua, XU Qihao, CHEN Liangzi, XIAO Guangming
    2023, 44(4):  994-1005.  doi:10.12382/bgxb.2021.0857
    Asbtract ( )   HTML ( )   PDF (20710KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    For large carbon fiber composite components used in aviation, increasing layer thickness and adding sacrificial layers are promising measures for controlling the deformation and improving assembly accuracy. However, milling a large number of sacrificial layers with high efficiency and no delamination damage is challenging. It is difficult to ensure that both the soft glass fiber protective layer on the surface and the hard carbon fiber composite sacrificial layers inside are free of burrs and delamination during the milling process. In this study, T800 carbon fiber reinforced polymer is used in a large aviation component as the research object. Milling experiments are carried out to analyze the effects of different machining parameters on milling quality, such as milling force, milling temperature, and machined surface roughness using four different structural tools. The experimental results indicate that the burr height of the machined surface decreases with the increase of spindle speed. When the feed speed and radial cutting depth increase, the burr height tends to increase. Higher milling temperature causes the deviation of fiber fracture position and increases the surface roughness. On the premise of ensuring the machining quality of carbon fiber composites, the sharp edge shape and multi micro edge milling method can significantly restrain the burr damages. The cutter with left-hand and right-hand micro edge structures make the milling process more stable.

    Research on Interference Mechanism of Swept-frequency Jamming to UWB Radio Fuze
    DONG Erwa, HAO Xinhong, YAN Xiaopeng, YU Honghai
    2023, 44(4):  1006-1014.  doi:10.12382/bgxb.2022.0088
    Asbtract ( )   HTML ( )   PDF (5205KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    An interference waveform pattern is studied for effective interference to UWB radio fuze. An interaction model of UWB radio fuze and periodically modulated interference signal are established. Based on the signal-to-interference ratio gain, the response characteristics of the fuze are analyzed under different noises, sine-wave amplitude modulation signals, sine-wave frequency modulation (FM) signals, and swept-frequency sinusoidal amplitude modulation (AM) signals. The simulated results are consistent with the theoretical values and verified by laboratory static confrontation tests. The results show that the swept-frequency AM interference is the most effective interference mode, and sine-wave AM interference is the best. By reasonably setting the parameters of the frequency sweep interference, the interference effect can be effectively improved.

    Microstructure and Properties of Laser Oscillating Welding with Filler Wire of Thin Wall Titanium Alloy T-joints
    WU Pengbo, XU Kai, HUANG Ruisheng, YANG Yicheng, ZOU Jipeng, CAO Hao
    2023, 44(4):  1015-1022.  doi:10.12382/bgxb.2021.0894
    Asbtract ( )   HTML ( )   PDF (12142KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    In laser oscillating welding with filler wire, heat input is a key factor affecting microstructures and properties of the welded joint. Therefore, investigating the relationship between heat input and microstructures and properties can provide data support and theoretical basis for improving thin-wall titanium alloy welded joints. In this study, laser oscillating welding with filler wire is to join a 2mm thick TC4 titanium T-shape joint, and the microstructures and mechanical properties of different zones are analyzed. The result show that the weld surface is well-formed, with no defects such as incomplete fusion, pores, or slag inclusions. The weld microstructures are mainly composed of α' martensite phase and primary β phase, with a small amount of twins and dislocations. The heat-affected zone is mainly composed of α phase and α' martensite phase that have not undergone phase transformation in the base metal. The hardness value of the welded joint fluctuates between 286 and 413HV, and that of the weld zone is the highest, 38% higher than the base metal. With the increase of welding heat input, more α' martensite is formed due to phase transformation, and the microhardness increases as well. The average tensile strength of the welded joint is 1076MPa, which is slightly higher than that of the base metal. The fracture of the tensile specimen occurs at the base metal and shows characteristics of the ductile fracture. The average shear strength of the welded joint is 679MPa. The fracture starting position of the shear specimen is inside the weld, and the fracture in the weld zone shows characteristics of intergranular fracture. The fracture in the heat-affected zone displayed characteristics of cleavage and quasi-cleavage trans-granular fracture.

    Long-Distance Aerial Target Detection Technology of Counter-UAV Image Seeker
    ZHAO Fei, LOU Wenzhong, FENG Huanzhen, SU Zilong, WANG Jinkui, XUAN Weikun
    2023, 44(4):  1023-1033.  doi:10.12382/bgxb.2021.0873
    Asbtract ( )   HTML ( )   PDF (8052KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    Taking the low-cost counter-UAV guided munitions as the research object, this study focuses on long-distance UAV target detection, and the design of a local visual saliency-based clustering measurement algorithm. In this algorithm, the idea of local contrast measurement is introduced into the visible light image for the first time, and the detection of the target by measuring the spectral clustering of the local imaging domain is realized.More specifically, it measures the minimum distance between the average spectral value of the local image domain and the spectral values of adjacent pixels. In addition, to solve the multi-scale target problem, a corresponding multi-scale sliding window measurement method is designed.The brief flow of the whole algorithm is as follows: frequency-division median filtering was performed on the original RGB image frame; to better measure the spectral difference, the filtered RGB image was converted to the Lab color space; the sliding window model was used for UAV imaging domain search; the saliency detection method was adopted to measure the spectral difference to obtain a saliency measurement map; finally, a thresholding algorithm was used to obtain the pixel position of the potential UAV target. According to the UAV target imaging conditions, field shooting and artificial synthesis of long-distance UAV image datasets were carried out. The experimental results showed that the algorithm can successfully separate the UAV target from the background under various complex meteorological conditions.

    Influence of Different Numbers of Rounds under Continuous Firing on Gun Barrel Life
    XU Yaofeng, WANG Jun, LIU Pengke, ZHU Wenfang, YANG Diao
    2023, 44(4):  1034-1040.  doi:10.12382/bgxb.2021.0852
    Asbtract ( )   HTML ( )   PDF (1491KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    The artillery is used with different charges of different types of ammunition (strong charge, full charge, reduced charge, high temperature charge, etc.), and have to undergo rapid continuous firing and performance test firing. It is necessary to study the impact of different charges of different types of ammunition and the number of rounds under rapid continuous firing on the barrel life. At present, for the assessment of barrel life, the method used is mainly to convert the number of projectiles of different types of ammunition into that of standard ammunition or standard ammunition with a specified ratio through the equivalent conversion factor in the national military standard. The existing national military standard equivalent conversion method for barrel life only includes two factors, chamber pressure and muzzle velocity, and does not consider the impact of rate of fire and number of rounds on barrel life, which makes it impossible to effectively evaluate barrel life under different numbers of rounds under continuous firing. The thermochemical ablation model of barrel material is established based on the Arrhenius equation. The influence of different numbers of rounds under continuous firing on the barrel life is studied. The larger the number of rounds under continuous firing, the shorter the barrel life. The accuracy of the thermochemical ablation model is verified by comparing the simulation and test results.

    A LOG Filter Based Enhanced Local Contrast Algorithm to Detect Infrared Small Targets
    MA Pengge, WEI Hongguang, SUN Junling, TAO Ran, PANG Dongdong, SHAN Tao, CAI Zhiyong, LIU Zhaoyu
    2023, 44(4):  1041-1049.  doi:10.12382/bgxb.2021.0767
    Asbtract ( )   HTML ( )   PDF (6959KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    To address the problem of high false alarm rate of single-frame infrared small-target detection algorithm in low-altitude and complex backgrounds, a Laplacian of Gaussian (LOG) filter-based enhanced local contrast algorithm is proposed. First, the candidate target pixels are extracted quickly by LOG filtering, while the target is enhanced using pixel grayscale indexing. Then, the target saliency map is calculated based on the grayscale features of the target and the background in the local area. Finally, the target is extracted by adaptive threshold segmentation. Test datasets are constructed for different low-altitude complex scenarios, and the proposed algorithm is compared with the Top-Hat algorithm, Max-median algorithm, RLCM algorithm, IPI algorithm, and MPCM algorithm in terms of signal-to-noise ratio gain, background rejection factor, detection rate, false alarm rate, and computational efficiency. Results show that in different scenarios, the newly proposed algorithm not only has higher signal-to-noise ratio gain and background rejection factor, but also has higher detection rate, lower false alarm rate and higher computational efficiency than other algorithms, demonstrating the method’s effectiveness and robustness.

    Mechanism of Dynamic Responses of Grillage Structures under Loads of Close-in and Contact Underwater Explosions
    SHEN Chao, ZHANG Lei, ZHOU Zhangtao, LIU Jianhu
    2023, 44(4):  1050-1061.  doi:10.12382/bgxb.2022.0037
    Asbtract ( )   HTML ( )   PDF (12574KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    This paper designs grillage structure models based on a specific protective structure of a surface ship, and conducts close-in and contact underwater explosion experiments on 10 grillage models under 7 working conditions with various charges and distances. The velocities of typical points are measured with the Photonic Doppler Velocimetry system, the fragments of the grillage structure are gathered, and the damage forms after each experiment are recorded. The experimental results compare well with the numerical results, verifying the generality of the experiment and the accuracy of the simulation. The analyses of experimental and numerical results reveal several conclusions. The grillage structure is susceptible to shear and tear at reinforcing ribs and diaphragm plates, leading to the formation of fragments. The number and weight of fragments depend on the explosive charges, distances, and structures of the grillage. The velocities of points on the surface of the grillage decrease exponentially with increasing distance between the measuring point and center point. The center point is the projection point of the explosive charge on the grillage surface. When the ratio of the explosion distance to explosive charge radius is not less than 2, the velocity of center point remains nearly constant, even though the explosive charge mass changes.

    The Kinematic Accuracy Reliability and Reliability Sensitivity Analysis of a Swing Mechanism with the Automatic Loading System of a Cannon
    ZHAI Wenyu, QIAN Linfang, CHEN Guangsong
    2023, 44(4):  1062-1070.  doi:10.12382/bgxb.2021.0868
    Asbtract ( )   HTML ( )   PDF (1907KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    This study aims to analyze the kinematic accuracy reliability of a swing mechanism with an automatic loading system and calculate the reliability sensitivity of dimension parameters. A kinematical model of the swing mechanism is thus established. Considering the influence of dimension error of the swing mechanism and joint clearance, the first four statistical moments are obtained by using the spare grid numerical integration method, and the probability density function of the kinematic response variable is obtained using the saddle point estimation method. The kinematic accuracy reliability of the swing mechanism with the automatic loading system is then calculated, and the reliability sensitivity analysis of dimension parameters is performed based on the results. The simulation results show that the calculation results in the study are identical to those acquired using the Monte Carlo method while requiring fewer sample points. The effectiveness of the methods in the paper is verified, and there is less failure probability of the swing mechanism kinematic accuracy, indicating high reliability in kinematic accuracy. The reliability sensitivity analysis of the dimension parameters reveals that the length of the driving arm has a larger influence on the kinematic reliability, while the other parameters have less influence. This provides references for the reliability-based design of the swing mechanism.

    Compound Control Method of ADRC and FNTSM for Airborne Object Tracking System
    GAO Yuxuan, HOU Yuanlong, GAO Qiang, HOU Runmin
    2023, 44(4):  1071-1085.  doi:10.12382/bgxb.2022.0890
    Asbtract ( )   HTML ( )   PDF (3552KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    Due to the influence of external disturbances, internal parameter perturbations and unmodeled dynamics, the design of the tracking control subsystem of the airborne object tracking system is faced with great challenges. A disturbance rejection control method is studied based on the optoelectronic stabilized two-axis four-gimbal platform. To solve the problems that the disturbance compensation of active disturbance rejection control (ADRC) is generally accompanied by disturbance residuals and that sliding mode control will introduce large chattering, a compound control method of ADRC and fast non-singular terminal sliding mode (FNTSM) control is designed. The linear extended state observer is employed to estimate the total disturbance and compensate it, thus allowing a smaller switching gain for the sliding mode when designing the control rate of sliding mode control, and fast non-singular terminal sliding surface is designed to obtain the control rate, which accelerates system convergence and avoids non-singular phenomena. The simulation results show that the proposed method can achieve high stability accuracy and introduce small chattering despite the influence of external disturbances and model uncertainties, which verifies the effectiveness of the compound control method.

    Effect of Detonation Instability and Initial Pressure on Track Angle of Spinning Detonation
    ZHAO Huanjuan, LIU Keqing, PANG Lei, LIU Jing, LIN Min, DONG Shiming
    2023, 44(4):  1086-1096.  doi:10.12382/bgxb.2021.0860
    Asbtract ( )   HTML ( )   PDF (8278KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    Experiments were conducted in the detonation tube with an inner diameter of 63.5mm to study the effect of initial pressure and detonation instability on track angle. In the detonation experiments, four typical premixed mixtures (which could be divided into stable mixtures such as Ⅰ:2H2+O2+50%Ar, Ⅱ:C2H2+2.5O2+85%Ar and Ⅲ:C2H2+5N2O, and unstable mixtures such as Ⅳ:CH4+2O2) were used. During the experiments, the cellular structure of the spinning detonation wave was recorded on the smoked foils. And then, the track angles α+ /α- between the right-handed/left-handed transverse waves and the tube axis were measured under different pressures. At the meantime, the variation of track angle and the influence of initial pressure and gas instability on track angle were analyzed. The results were obtained as follows. The track angles of the four premixed mixtures were in the range of 30°~50°. For the gases (Ⅰ, Ⅱ, Ⅲ) with relatively weak detonation instability, the measured values of track angle were in good agreement with theoretical values. However, for the gas with high instability (Ⅳ), the agreement was poor. The magnitude and variation trend of the dispersion of track angle was consistent with those of the cellular structure dispersion. In addition, the higher the initial pressure, the smaller the track angle. As the initial pressure increases, the track angles of the four premixed gases were all significantly decreased, and the decrease was basically consistent. Finally, in the high-frequency spinning phase, the effect of initial pressure on track angle was stronger than that of detonation instability.

    Key Technology for Ultrasonic Measurement of Burning Rate in Large-scale Solid Rocket Motors
    SUN Dechuan, XIAN Guang
    2023, 44(4):  1097-1106.  doi:10.12382/bgxb.2021.0805
    Asbtract ( )   HTML ( )   PDF (7570KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    Measuring the true burning rate of a solid rocket motor (SRM) is a challenging problem in SRM research and development. Ultrasonic measurement has been proven to be a feasible solution. This study provides an overview of the related technologies for measuring dynamic and large-scale motor burning rates using ultrasonic technology. Static tests of steel shell/propellant assembly and high-temperature verification tests of the steel shell solid motor are carried out using low-frequency ultrasonic technology. After review and experimental verification, it is determined that low-frequency ultrasonic is the most feasible approach for measuring the burning rate of large-scale SRM. A further research direction is to optimize the probe layout. The study also provides suggestions for ultrasonic data processing.

    Firing Process Modeling of a Soft Recoil Gun Based on Interval Uncertainty Parameter Identification
    GUO Shuqi, HOU Baolin
    2023, 44(4):  1107-1117.  doi:10.12382/bgxb.2021.0885
    Asbtract ( )   HTML ( )   PDF (4289KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    The soft recoil firing technology is a significant way to reduce the recoil force of a gun. A new multi-port recoil mechanism with a central port and variable-depth wall grooves is proposed to investigate the firing characteristics of a soft recoil gun. The flow distribution Bernoulli equation is established with CFD simulation to improve the model accuracy. On this basis, the interval uncertainty theory and genetic algorithm are applied to build the parameter identification model of the firing process. The typical parameters of the soft recoil gun are identified and obtained with the test data of the first round. The similarity rate between the simulation and test data can reach up to 92.78%. Moreover, the corresponding simulation results match the test data through the second and the third round. It is proved that the correct modeling and effective identification results provide theoretical guidance for the design of a soft recoil gun.

    Thermal Reactivity and Combustion Performances of Al/Ti-based Nano-composite Fuels
    YANG Sulan, ZHANG Haorui, NIE Hongqi, YAN Qilong
    2023, 44(4):  1118-1125.  doi:10.12382/bgxb.2022.0132
    Asbtract ( )   HTML ( )   PDF (6574KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    To effectively promote the intermetallic reaction between Al and Ti, two types of core-shell structured nanocomposite fuels have been prepared by using the high-energy ball milling method, namely Al/Ti@AP/NC and Al/Ti@PVDF/CL-20. The quality of the coating layers of AP/NC and PVDF/CL-20 on the surface of Al/Ti is inspected by scanning electron microscopy (SEM). The thermal reactivity, heat of reaction and combustion performances of Al/Ti-based composite fuels are evaluated by DSC/TG thermal analyses, a bomb calorimeter, and a customized combustion diagnostic system. The morphologies and compositions of the condensed combustion products (CCPs) are characterized by SEM and X-ray diffraction (XRD) techniques, respectively. Results show that the core-shell structured Al/Ti@AP/NC and Al/Ti@PVDF/CL-20 could be obtained by high-energy ball milling method. The thermal decomposition of the energetic composites is enhanced with the introduction of Al/Ti. Furthermore, the intermetallic reaction between Al and Ti, burning rate, and the combustion wave temperature could be enhanced with the inclusions of AP/NC or PVDF/CL-20. In particular, for the composite fuel coated with AP/NC, the burning rate (246.6mm·s-1) is increased by 9.5 times and the combustion wave temperature (1703.2℃) is 59.3% higher compared to that of pure Al/Ti (the burning rate and combustion wave temperature are 23.5mm·s-1 and 1069.3℃, respectively). The compositions of the CCPs depend on the types of energetic coating layers, which are dominated with AlTi2C and Ti(O0.19C0.53N0.32), indicating that chemical reactions occur between Al/Ti and energetic composites during the combustion process.

    Load Characteristics of High Chamber Pressure and High Speed Launch of Underwater Vehicle
    LIU Yue, ZHAO Zijie, DAI Qi, WANG Anhua, ZHANG Hui
    2023, 44(4):  1126-1138.  doi:10.12382/bgxb.2021.0802
    Asbtract ( )   HTML ( )   PDF (9566KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    The multiphase flow field formed behind a vehicle under high-chamber pressure and high-speed launch in water is complex, and the load effect is not clear yet. The launch load characteristics of a small-caliber underwater vehicle during cold launch under high chamber pressure and high initial velocity were investigated. The flow field and dynamic characteristics during interior ballistics, interaction between overflow gas and water, and hydrodynamic ram effect stage during the launch of the vehicle were analyzed. A numerical model of the high-speed cold launch process of the underwater vehicle was established, while a numerical multicomponent gas-vapor-liquid simulation was performed using a multiphase flow model and a dynamic grid approach. The load characteristics of launcher and their causes in different phases were then analyzed. The results showed that: large impact loads were mainly from the internal ballistic process and the hydrodynamic ramhydrodynamic ram effect, while a relatively small load was from the low-pressure area caused by overflowing gas; more specifically, the hydrodynamic ram hydrodynamic rampeak pressure decreased significantly because the mixed gas spilled out in large quantities under high chamber pressure, which was different from the low chamber-pressure launch condition.

    Theoretical Calculation of IgnitionLocation and Temperature for One-Dimensional Slow-Cook Model
    ZHANG Kun, ZHI Xiaoqi, XIAO You, WANG Shuai
    2023, 44(4):  1139-1147.  doi:10.12382/bgxb.2022.0599
    Asbtract ( )   HTML ( )   PDF (4879KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    To theoretically analyze the slow-cook process of condensed explosives and lay a theoretical foundation for the study of cook-off, based on the theoretical equation for heat conduction of explosives, the non-reactive heat conduction and self-heating reaction heat conduction of explosives are separated by using the superposition principle and the method of separating variables. Therefore, an analytical solution of temperature distribution for one-dimensional slow-cook model of condensed explosives is derived. The variation of the location of the maximum temperature of the self-heating reaction with heating time is calculated and studied, along with the variation of maximum temperature of self-heating reaction and temperature gradient with thickness. According to the results of the slow-cook test, the temperature distribution along the axial direction is verified. The ignition position, ignition temperature and ignition time are verified by numerical calculation. The results show that the ignition position determined by theory is consistent with the measured result by experiment. The calculation results determined by theory are consistent with the numerical calculation results. As far as one-dimensional RDX explosives is concerned, the location change of the maximum temperature is less than 2% from beginning to ignition, which can be ignored. Therefore, the location of the maximum temperature of self-heating reaction of explosives is almost unchanged during the slow-cook process. When the thickness of explosive reaches 0.3m, with the increase of the explosive thickness, the distance from the ignition position to the boundary tends to be a constant value of 0.015m. The temperature gradients inside these explosives are similar.

    Research on Characteristics of Abnormal Underwater Acoustic Wave Transmission through Water-Air Interface
    QIANG Wei, LI Ning, HUANG Xiaolong, KANG Yang, LI Can, WENG Chunsheng
    2023, 44(4):  1148-1157.  doi:10.12382/bgxb.2021.0891
    Asbtract ( )   HTML ( )   PDF (5954KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    To explore the abnormal transmission characteristics of underwater acoustic wave through the water-air interface, theoretical and experimental studies on abnormal acoustic transmission under the effect of inhomogeneous waves are carried out. An underwater acoustic wave transmission experiment system is constructed in both the laboratory and the open water environment of Qiandao Lake.The law of the transmission coefficient with the depth of the sound source and the frequency of the sound wave are obtained.The mechanism and influencing factors of the inhomogeneous waves are thoroughlyanalyzed.The results demonstrate that when the product of source depth and underwater sound wave number is less than 1, the effect of inhomogeneous waves cannot be ignored, and the transmission coefficient increases abnormally.When the energy ratio of the homogeneous waves and inhomogeneous waves is close, the transmission coefficient decreases undulatingly with the increase of the wave frequency, and decreases smoothly with the increase of the source depth.The range of radiation angles of underwater acoustic waves transmitted into the air is greatly affected by the inhomogeneous waves.With a stronger inhomogeneous wave effect, the radiation angle range gradually expands. The research results lay afoundation for applyingabnormal transmission of underwater acoustic waves in the real world,and provide data support for the transmission of acoustic signals across media.

    Influence on Flow Field of Hot Launch in a W-Shaped Underground Space by Water Injection
    ZHANG Manman, JIANG Yi, SHI Shaoyan, DENG Yueguang
    2023, 44(4):  1158-1170.  doi:10.12382/bgxb.2022.0014
    Asbtract ( )   HTML ( )   PDF (10483KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    The water spray system is used to improve the flow field in the thermal launch process of missiles in underground spaces, with the aim of reducing the peak value of pressure pulse, alleviating pressure oscillation, and reducing the temperature of flow field through “decompression and cooling”. In this study, a gas-liquid two-phase flow control equation is established by combining the three-dimensional viscous compressible Navier-Stokes equation, mixture multiphase flow model, and phase change model. The mathematical model and numerical method are validated using gas jet scaling test data. Computational fluid dynamics (CFD) numerical calculation method is used to analyze the influence of the water spray system on the flow field environment during the missile’s underground space launch process. The results show that the environmental characteristics of the flow field in the underground space during the thermal launch of the missile are effectively improved by establishing a water spray system at the bottom of the W-shaped underground space. The water spray system has a good suppression effect on the initial overpressure phenomenon. The bottom pressure oscillation is reduced from 8 times to 4 times. The pressure changes slowly up and down at 1 atm, with the maximum pressure only about 1.20×105Pa. The initial overpressure peak is reduced, and the frequency and amplitude of the pressure oscillation are reduced, achieving the decompression effect. Through the process of violent vaporization of liquid water and momentum exchange, the phenomenon of gas backsplash is strongly and effectively suppressed by the water spray system. The gas is confined at the bottom of the cylinder, and the maximum temperature at the bottom of the missile is reduced from 3000K to about 400K, achieving the “cooling” effect.

    Feature Extraction and Region Growing Algorithm for Processing CT Scans of Engine Parts
    ZHANG Bin, LU Hongyi, LIU Shun, SANG Doudou, YANG Yucheng
    2023, 44(4):  1171-1180.  doi:10.12382/bgxb.2021.0893
    Asbtract ( )   HTML ( )   PDF (3080KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    Aiming at the problem that the influence of metal artifacts and noise in industrial computed tomography (CT) images will interfere with the accuracy and precision of part segmentation extraction, a feature extraction method based on standard deviation weight threshold and region growing is proposed for industrial CT images. A two-dimensional maximum between-class variance and two-dimensional minimum cross-entropy threshold segmentation algorithm based on standard deviation weight is proposed to remove the image background. Automatic selection of various sub-point regions is made based on the neighborhood mean of the image. The extraction of component features is completed based on the Scharr operator to calculate the gradient and improve the growth criterion. Experimental results demonstrate that compared with other region growing methods, our algorithm improves accuracy by 9.1% and achieves a maximum pixel accuracy close to 1. The dice score improves by 5.3% while the intersection over union is improves by 4.1% at maximum. Our feature extraction algorithm outperforms other region growing methods.

    High-Speed Two-Dimensional Measurements of Flame Propagation Velocity and Temperature Distribution of TiH2 Dust Flame
    CHENG Yangfan, WANG Zhonghua, HU Fangfang, ZHANG Beibei, XIA Yu, SHEN Zhaowu
    2023, 44(4):  1181-1192.  doi:10.12382/bgxb.2021.0842
    Asbtract ( )   HTML ( )   PDF (10070KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    In order to explore the application feasibility of hydrogen storage alloy TiH2 in thermobaric bombs, an open and a semi-open Hartmann tube were used to simulate the explosion processes of a thermobaric bomb in the air and underground tunnels, respectively. By using the two-dimensional high-speed measurement platform on basis of the colorimetric thermometry and contour detection methods, flame characteristic parameters and influencing factors of TiH2 dust cloud with different concentrations were studied. The experimental results showed that: in the open space, the flame temperature of TiH2 dust was in the range of 2150-2400K, and the flame temperature decreased with the increase of dust concentration; the flame propagation velocity and acceleration were not affected by the dust concentration in the early stage, but increased with the increasing dust concentration in the later stage; in the confined space of a pipeline, the temperature of dust clouds with different concentrations of TiH2 during stable combustion were around 2430K, and the higher the dust concentration, the shorter the flame propagation time to the top; the stable flame temperature of dust clouds in the pipeline was 50-210K higher than that in the open space, and the flame propagation velocity was 6-15 times than that in the open space. Compared with the traditional explosion testing methods, the colorimetric thermometry method can precisely measure the transient temperature distribution of a certain zone, and the contour detection method can accurately measure the propagation velocity and acceleration of flame front surface, which may provide a new technical means for the formulation design and damage effectiveness evaluation of thermobaric bombs.

    Study on Orthogonality of Light Vector Trajectory of 45 ° Scanning Mirror in Fine Pointing Mechanism
    LI Xiangyang, LI Xiangyue, SUN Xueping, ZHANG Jiahua, REN Bin, ZHANG Xuejiao, CHEN Anhe, CHEN Xiang, ZHANG Wenrui
    2023, 44(4):  1193-1199.  doi:10.12382/bgxb.2021.0876
    Asbtract ( )   HTML ( )   PDF (3253KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    In the laser communication terminal in space, the scanning trajectory on the CMOS camera is not orthogonal when the fine pointing mechanism of the 45° scanning mirror vibrates around different shaft systems, which reduces the scanning probability and makes it more difficult to calibrate the optical axis of the laser terminal in orbit. In order to solve this problem, the ray tracing method is used to establish a three-dimensional light vector scanning trajectory model, and the orthogonality of the light vector trajectory on the CMOS camera is calculated and simulated when the vibration axis of the 45° mirror scans along two sets of commonly used orthogonal axes. Then, an experimental test system is built to verify the performance of the reflected light vector in the scanning process of the fine pointing mechanism. The results show that: the non-orthogonality of the 45° scanning mirror vibrates around P=(1/2,-1/2, 2/2)T and P'=(1/2,-1/2,- 2/2)T is 19.47°, and the included angle of the scanning trajectory on the CMOS camera changes with the scanning angle according to the relationship between the scanning angle and the orthogonality curve of the scanning trajectory; the non-orthogonality of the scanning trajectory is 6.4 mrad when the scanning angle is 9 mrad. This study provides insights into the internal mechanism and has guiding significance for the installation mode and optical axis calibration of the off-axis field of view of the fine pointing mechanism of space laser communication terminal.

    A Method for Calculating the Shielding Effectiveness of Radio Fuze Cavity
    CHEN Kaibai, GAO Min, ZHOU Xiaodong, BI Junjian, WANG Yi
    2023, 44(4):  1200-1208.  doi:10.12382/bgxb.2021.0888
    Asbtract ( )   HTML ( )   PDF (3958KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    The internal space of radio fuzes is limited, making it difficult to measure the electromagnetic shielding effectiveness (SE) of their cavity through experiments. To analyze the SE of the radio fuze cavity under the circumstance of a strong electromagnetic pulse, a calculation method on electromagnetic topology theory and Baum-Liu-Tesche (BLT) equation is proposed in this paper. This method establishes the cavity propagation matrix by analyzing the energy flow characteristics, calculates the cavity scattering matrix by using the equivalent circuit model, deduces the extended BLT equation of energy transmission in the cavity, and then obtains the voltage value of each topological node. The effectiveness of this method is verified using CST software. The SE of various models, including the rectangular antenna window model, circular antenna window model, double-sided circular hole model, and dielectric substrate model, is calculated. The calculation results are analyzed quantitatively using the correlation coefficient, and the results show that the calculation accuracy of the proposed method is better than that of the equivalent circuit method. The needed calculation memory is lower than that of the CST software. This method can be used to analyze the SE of fuzes with cylindrical cavities.

    Phase-switched Screen Periodic Non-uniform Intermittent Modulation Method
    KONG Yameng, WANG Guoyu, FENG Dejun, WANG Junjie
    2023, 44(4):  1209-1216.  doi:10.12382/bgxb.2021.0789
    Asbtract ( )   HTML ( )   PDF (4159KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    Phase-switched screen (PSS), as a kind of artificial electromagnetic material with dynamically adjustable electromagnetic scattering characteristics, can change radar target characteristics by controlling the reflection state of electromagnetic waves to realize radar target simulation or false target generation. To address the problem of limited control parameters and single modulation effect of the phase-switched screen periodic intermittent modulation method, a phase-switched screen periodic non-uniform intermittent modulation method is proposed. The periodic non-uniform intermittent modulation signal model is constructed on the basis of the periodic intermittent modulation signal, the modulation coefficient is introduced according to the characteristics of the modulation signal, and the dimension of the phase-switched screen control parameter is expanded. Through theoretical derivation, the influence of the PSS periodic non-uniform modulation method on the radar chirp signal is analyzed. The simulation experiment results show that compared with the PSS periodic intermittent modulation method, this method has more flexible modulation styles and more diverse modulation results, thus having higher application value in radar target simulation and radar target characteristic control.

    Applications of Hovering Deep Bombs Based on Predetermined Probability
    WU Ling, WANG Pikun, LU Faxing
    2023, 44(4):  1217-1224.  doi:10.12382/bgxb.2022.0005
    Asbtract ( )   HTML ( )   PDF (1474KB) ( )  
    Figures and Tables | References | Related Articles | Metrics

    When using hovering deep bombs to intercept incoming torpedoes, multiple deep bombs are deployed along the possible torpedo path to form an interceptor line, thus increasing the probability of damaging the torpedo. The traditional deployment method is based on the detection error of the torpedo and the radius of destruction of the deep shells. It determines the probable passage interval of the target and distributes the deep shells evenly. However, the traditional method does not take into account the firing error of the deep ammunition or allow for a reasonable number of deep ammunition deployments and aiming points based on a predetermined damage probability. To address this, an optimal interception model is constructed by taking the destruction probability as the predetermined index, considering both observation error and firing error. By constructing an intermediate function, the theoretical optimal damage probability is obtained, and the predetermined damage probability is used as input for iteratively solving the number of deep bombs to be deployed based on the optimal damage probability. Finally, the targeting point of deep bomb deployment is determined by analyzing the interception strategy. Simulation calculations show that this method can quickly obtain the optimal number of projectiles and aiming points based on the predetermined firing probability. The error between the verified damage probability and the predetermined damage probability of the scheme is less than 1%, achieving the accurate deployment of the underwater interception line.