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    30 March 1985, Volume 6 Issue 1
    Paper
    Extension of Volterra Equations to Non-linear non-holonomic Mechanical Systems
    Mei Fengxiang
    1985, 6(1):  1-10.  doi:10.3969/j.issn.1000-1093.1985.01.001
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    In this paper,Volterra equations for linear non-holonomic systems are extended to non-linear non-holonomic systems, and the generalized Volterra equations are obtained, Two examples are given. The generalized Yolterra equations are transformed to ones expressed in terms of the generalized coordinates.
    The Formula of The Random Wind Dispersion of The Unguided Unguided Unstable Finned Rocket and The principle of Zero Wind Dispersion
    Liu Yixin
    1985, 6(1):  11-16.  doi:10.3969/j.issn.1000-1093.1985.01.002
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    In this paper,the formula of the random wind dispersion of the unguided unstable finned rocket was derived. Then using digital computer, the table of characteristic function for engineering calculation was given. In total dispersion,the random wind dispersion of the unguided finned rocket is very important. Therefore,in this paper,the principle of the zero wind dispersion was suggested, i. e. in a confined period cift6r th.6 iEunch. of the rocket, the folded fins of tke rocket spread out.
    Non-linear Random Vibration of The Vehicle Suspended With Oil-Pneumatic Spring
    Lin Yaoqun, Xi Dechang
    1985, 6(1):  17-25.  doi:10.3969/j.issn.1000-1093.1985.01.003
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    In this paper,the vibration of the vehicle suspended with oil-pneumatic springs is investigated, simplified as a two-degree non-linear system subjected to a stationary random road excitation. The MSRs of the displacement,velocity and acceleration of the vehicle vibration are given. The approach of selecting oil-pneumatic spring parameters is proposed.

    A Method for Calculating The Optimal Fit Ballistic Coefficient
    Ma Dianrong
    1985, 6(1):  26-32.  doi:10.3969/j.issn.1000-1093.1985.01.004
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    The problem to be studied in this paper is how to calculate the optimal fit ballistic coefficient from given coordinates of a trajectory under the condition of constant ballistic coefficient. This is a practical problem in construction of firing tables and in other calculation of exterior ballistics. First of all, the definition of the optimal fit ballistic coefficient and the mathematical description of the problem are pointed out; and the problem is reduced further to a optimization of two variables. Then,the calculation method of the optimal fit ballistic coefficient is narrated and the block diagram of the programming is designed correspondingly. Finally,some examples are recounted in order to show the feasibility of the calculation method mentioned' in this paper.
    Modelling in The Process of The Perforation of Projectile into A Target
    Gao Juxian,Le Maokang, Lu Deye, Xie Baomin, et al
    1985, 6(1):  33-39.  doi:10.3969/j.issn.1000-1093.1985.01.005
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    This paper discusses a similarity method in the perforation of the projectile into a target. First of all, various physical quantities and similarity parameters which determine the process of the perforation are analysed. Then on the basis of the analysis geometrical similarity law is discussed and verified for both of blunt-nose-projectile and long-rod-projectile.

    Syntheses of Nitroderivatives of Hydrazines
    Jiang Delin
    1985, 6(1):  40-44.  doi:10.3969/j.issn.1000-1093.1985.01.006
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    N-methyl-N, Nˊ-bis(trinitroethyl) hydrazine was prepared by reaction of methylhydrazine with formoldehyde and nitroform. The nitration of the obtained compound gave N-methyl-Nˊ-nitro-N,Nˊ-bis (trinitroethyl) hydrazine. The structure of the latter was verified by elementary analysis, molecular weight determination,IR,NMR. Reaction of carbohydrazide and 2,2 -dinitro-propenedial- 1,3 gave 1,2,4,5-Teraza-7,7-dinitro-bicyclo ( 3,3,1 ) nonanone-3. Its structure was verified also.
    Experimental Techniques and Analysis
    The Effect of The Engine Discharging Jet on The Aerodynamic Performance of Vehicles
    Yang Daowei
    1985, 6(1):  45-50.  doi:10.3969/j.issn.1000-1093.1985.01.007
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    Based on fundamental theory of gas dynamics,this paper generally discusses the effect of the engine discharging jet on the flow oyer vehicle, and analyses the wind tunnel experiments in which compressed air is substituted for high temperature discharging gas jet to find out its effect on the flow over vehicle. Experimental results are also presented and analysed.
    Research Notes
    Solubility and Apparent Viscosity of NC Concentrate Solution System
    Ren Yuli, Chen Shaozhen
    1985, 6(1):  51-54.  doi:10.3969/j.issn.1000-1093.1985.01.008
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    The solubilities of concentrate solution system composed of No. 3 nitrocellulose (NC) with dietyl phthalate (DEP),dibutyl phthalate (DBP) and glycerin triacetate(TA)have been studied in this paper. From the results of these experiments it is concluded that the order of their solubility is NC-DEP>NC-TA>NC-DBP. The solubilities of concentrate solution system of NC-DEP increase with the increase of its solvent ratio. The solubility of NC-mixed solvent system is better than that of NC-mono-sol- vent system. These results have some reference for designing and processing powders。

    An Exact Solution for The Stability Problems of Rectangular Plates Simply Supported under The Action of Unequal Uniform Loading in Two Mutually Perpendicular Directions
    Zhao Dongming, Xue Dawei
    1985, 6(1):  55-61.  doi:10.3969/j.issn.1000-1093.1985.01.009
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    Based on the stability concept of the non-linear theory of elasticity, this paper derived the formula of critical load for the buckling of rectangular plates simply supported on all four sides under the action of unequal uniform loading in two mutually perpendicular directions. The special case of the formula under the action of uniform loading only in one direction is emphatically investigated, and the relevant approximate formula convenient for applying to engineering practice is obtained. Moreover, the comparison with the corresponding solution in the classical theory of thin plates and the analysis for several numerical value calculated are also discussed.

    The Limit Cycle of Planar Non-linear Motion of Finned Projectile
    Han Zipeng
    1985, 6(1):  62-67.  doi:10.3969/j.issn.1000-1093.1985.01.010
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    In this paper, non-linear motion of finned projectile with small damp and weak non-linear static moment has been studied. Using the stable limit cycle,it has been explained that some finned projectiles probably produce self—oscillation. Using the unstable limit cycle,the causes of the fortuitous fall of some finned projectiles have been discussed. In order to decrease the influence of the self-oscilation and eliminate the fortuitous fall of the finned projectile? the non-linear part of the damping moment and lift must be inc— reased,and the non-linear part of the drag must be decreased.