Numerical simulation of a supersonic flow around finned boost vehicles

1Timoshenko, VI, 1Galinskiy, VP
1Institute of Technical Mechanics of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine, Dnipropetrovsk, Ukraine
Space Science and Technology 2017, 23 ;(5):33-43
https://doi.org/10.15407/knit2017.05.033
Section: Space-Rocket Complexes
Publication Language: Russian
Abstract: 
We describe the developed software that can be used for operative project calculations of the supersonic flow around finned boost vehicles.
Keywords: aerodynamics, boost vehicle, explicit finite difference schemes, gas dynamic equations, local interaction method, march multizone method, supersonic flow, thin panel
References: 
1. Wodlou A. B., Solo-mon Dj. M., Baltakis F. P. Calculation of supersonic inviscid flows near the bodies of type of finned missiles. AIAA J., 19 (N 9), 83—93 (1981).
2. Galinsky V. P., Timoshenko V. I. Calculation of the supersonic flowing around of bielliptic body with wings. Scientific messages of TSAGi, 9 (N 6), 48—55 (1978).
3. Galinsky V. P., Timoshenko V. I. Numeral research of supersonic stream near a bearing body with wings. Space researches on Ukraine, 89—92 (1981).
4. Galinsky V. P.,Timoshenko V. I. Results of numeral research of the supersonic flowing around of bodies with the wings of variable-swept. Applied questions of aerodynamics of aircrafts, 77—81 (Naukova Dumka, Kyiv, 1985).
5. Galinsky V. P.,Timoshenko V. I. Results of numeral research of the supersonic flow around of bodies with the wings of variable-swept. Aerothermodynamics of the aerospace systems. Collection of Lectures of Schoolseminar of TSAGi., Part II, 116—131 (TSAGi, 1992). – 30.01-4.02.1990.
6. Galinsky V. P., Timoshenko V. I. Problems in developing scientific methods for calculating aerodynamic parameters of boost vehicles. Space science and technology, 4 (N 2/3), 64—72 (1998).
https://doi.org/10.15407/knit1998.02.064
7. Godunov S. K., Zabrodin A. V., Ivanov M. Ja., et al. Numeral decision of multidimensional of gas dynamics tasks, 400 p. (Science, M., 1976).
8. Kolgan V. P. Application of principle of minimum values of derivative to the construction certainly — difference shemes for the calculation of break decisions of gas dynamics. Scientific messages of TSAGi, 3 (N 6), 68—77 (1972).
9. Rodionov A. V. Monotonous shemes the second order to approximation for the through calculation of non-equilibrium flows. J. comp. math. and math. phys., 27 (N 4), 565—593 (1987).
10. Rozin A. V. Research of flowing around of finned body the supersonic stream of gas. Aerodynamics of entrance of bodies in the atmosphere of planets, 17—23 (Publishing house MSU, M., 1983).
11. Timoshenko V. I. Supersonic flow of viscous gas, 187 p. (Naukova Dumka, K., 1987).
12. Timoshenko V. I. Computer simulation of Hyper- and supersonic aerogasdynamics flying vehicles. Aero-dynamics: Problems and Perspective. Collection of articles,
158—175 (National Aerocom. University «Kharkiv. aviation.in-t», Kharkov, 2004).
13. Timoshenko V. I., Galinsky V. P. Operative calculation of the spatial supersonic flowing around of bodies near to axisymmetrical. News of Institutions of Higher Learning. Aerotechics, N 4, 22—26 (1991).
14. Timoshenko V. I., Galinsky V. P., Bilotserkovets I. S. Problems of mathematical design of processes of aerogasdynamics of boost vehicle. Announcer of the Dnepropetrovsk university. Mechanics, 1 (N 1), 100—115 (1998).
15. Timoshenko V. I., Galinsky V. P., Bilotserkovets I. S., Zagniy V. V. Imitation design of processes of aero-gasdynamics of boost vehicles and choice of project parameters. Space-rocket Technique: Fundamental and Applied Problems: Labours of 2-nd international conference (18—21 November 2003 year), Part I, p. 169—178 (Publishing house MSTU named after N. E. Baumana, M., 2005).