DYNAMIC ANALYSIS of a BALLISTIC MISSIBLE MODEL

Authors

  • V. I. Pegov South Ural Scientific Centre of the Ural Division of RAS
  • I. Yu. Moshkin South Ural Scientific Centre of the Ural Division of RAS

DOI:

https://doi.org/10.14529/mmp170406

Keywords:

missile model, hydrodynamics, hydraulic device, test, air chamber.

Abstract

A hydraulic catching device in the form of a blind water-lled pipe is widely used to ensure safety in tests of ballistic missile models in hydrodynamic test tanks. An air chamber is provided at the pipe end wall to avoid a water-hammer eect. The developed math model and methodology for analyzing dynamics of a ballistic model in a hydraulic catching device permit to choose geometrical parameters of a catching device and decelerate the model in preset design conditions. The model longitudinal equation was derived from the Lagrange equation. The proposed methodology was used to create a software program and make trial calculations. The calculation data were compared with the experimental ones obtained during tests in a hydrodynamic tank. The calculation and experimental data are in good compliance proving adequacy and reliability of the developed math model for a deceleration hydrodynamic device. In case of the given Euler number and model mass, the developed math model allows choosing basic parameters of a catching decelerating device which are required for deceleration. The proposed methodology can be used to dene geometrical parameters of a decelerating and catching device for testing a ballistic model in a hydrodynamic tank.

Author Biographies

V. I. Pegov, South Ural Scientific Centre of the Ural Division of RAS

Doctor of Engineering Sciences

I. Yu. Moshkin, South Ural Scientific Centre of the Ural Division of RAS

Candidate of Engineering Sciences

References

Degtiar V.G., Pegov V.I.Gidrodinamika podvodnogo starta raket[Hydrodynamics of Rocket Launches from Underwaters], Ìoscow, Machinostroyeniye, 2009. (in Russian)

Pegov V.I., Moshkin I.Yu.Metod raschyota dinamiki ballisticheskoy modeli v gidrobasseyne[A Methodology for Analyzing Dynamics of a Ballistic Model in a Hydrodynamic Tank], Miass, SUSU Electrical Engineering Department, 2016. (in Russian)

Pegov V.I., Cheshko A.D., Moshkin I.Yu, Merkulov Ye.S. [Experimental Modelling and Simulation of Launching Effect on a Submarine].Vzglyad v budushchee - 2016[A Look into

the Future 2016], CDB ME "Rubin", Saint Petersburg, 2015, pp. 553-560. (in Russian)

Benevolski S.V., Burlov V.V., Kazakovski V.P.Ballistika[Ballistics], Penza, Penza artillery engineering institute, 2009. (in Russian)

Dmitrievskiy A.A., Lysenko L.N.Vneshnyaya ballistika[External Ballistics]. Moscow, Machinostroyeniye, 2005. (in Russian)

Lysenko L.N.Navedeniye i navigatsiya ballisticheskikh raket[Guidance and Navigation of Ballistic Missiles]. Moscow, Izd-vo MGTU im. N.E. Baumana, 2007. (in Russian)

De Molleson G.V., Stasenko A.L. [Flow Around the Body with a Gas-Dispersed Jet in a Wide Range of Values of the Braking Parameters].Teplozika vysokikh temperature, 2017, vol. 55,

no. 1, pp. 94-108. (in Russian)

Pakhomov M.A. [Infuence of Evaporation of Droplets on Gas Turbulence and Heat Transfer During a Two-Phase Flow Behind a Sudden Expansion of a Pipe].Teplozika vysokikh temperature, 2016, vol. 54, no. 3, pp. 352-366. (in Russian)

Published

2017-12-08

Issue

Section

Mathematical Modelling