Source: http://knit.mao.kiev.ua/en/archive/1998/2/12
Timestamp: 2019-04-20 02:20:32+00:00

Document:
We discuss the problems that arise in the development of scientific methods for calculating aerodynamic characteristics of boost vehicles. We describe briefly the methodology and the software developed at the Institute of Engineering Mechanics NASU and the National Space Agency of Ukraine for aerodynamic calculations of boost vehicles in the «Svityaz-1» and «Oril» projects of the space program of Ukraine.
1. Belotserkovets I. S., Timoshenko V. I., Filippovskaia L. M. Effect of the nonuniformity of external supersonic flow and nozzle deflection angle on the base pressure behind an axisymmetric body with a single supersonic jet. Izv. VUZov. Aviatsionnaia Tekhnika, No. 1, 34—36 (1990) [In Russian].
2. Voronova G. G., Limanskii A. V., Timoshenko V. I. A parametric study of the lift-drag ratio of blunt cones. TsAGI, Uchenye Zapiski, 22 (1), 77—81 (1991) [In Russian].
3. Galinskiy V. P., Timoshenko V. I. The results of numerical investigation of supersonic flow of bodies with variable sweep wings. In: Applied aerodynamics of aircraft., 77—81 (Nauk. dumka, Kiev, 1985) [In Russian].
4. Galinskiy V. P., Timoshenko V. I. The results of numerical investigation of supersonic flow of bodies with variable sweep wings. Aerothermodynamics of aerospace systems: Sb. dokl. shkoly-seminara CAGI, Pt. II, 116—131 (Izd-vo CAGI, Moscow, 1992) [in Russian].
5. Godunov S. K., Zabrodin A. V., Ivanov M. Ia., et al. Numerical solution of multidimensional problems of gas dynamics, 400 p. (Nauka, Moscow, 1976) [In Russian].
6. Kushnir G. G., Timoshenko V. I. Parametric issledo¬vanie aerodynamic drag and the elliptic-quality Biel blunt cones. Izv. VUZov. Aviatsionnaia Tekhnika, No. 2, 67—68 (1989) [in Russian].
7. Rozin A. V. Study flow feathered body supersonic gas flow. In: Aerodynamics of re-enter into the atmosphere of planets, 17—23 (Izd-vo MGU, Moscow, 1983) [In Russian].
8. Timoshenko V. I. Application package of integrated solutions of problems of supersonic flow around axisymmetric bodies . In: Complexes mathematical physics programs, 52—60 (Izd-vo ITPM SO AN SSSR, Novosibirsk, 1980) [In Russian].
9. Timoshenko V. I., Belotserkovets I. S. Numerical simulation of supersonic spatial flow around blunt bodies. In: Fluid Dynamics and Heat and Mass Transfer of aircraft, 53—58 (Nauk. dumka, Kiev, 1988) [In Russian].
10. Timoshenko V. I. , Galinskiy V. P. Operational calculation of spatial supersonic flow of bodies, close to axially symmetric. Izv. VUZov. Aviatsionnaia Tekhnika, No. 4, 22—26 (1991) [In Russian].
11. Timoshenko V. I. , Galinskiy V. P. , Belotserkovets I. S. Problems of scientific and methodological support of the aerodynamic development of launch vehicles. In: Scientific and technical problems of astronautics and rocketry: Tez. i annotacii dokl. metodich. konf., 96—97 (Izd-vo CNIIMash, Moscow, 1996) [In Russian].
12. Timoshenko V. I., Limansky A. V. Numerical Computer Solution Technology for Gas-Dynamics Problems, 231 p. (Naukova Dumka, Kiev, 1985) [in Russian].
13. Timoshenko V. I., Filippovskaia L. M. Numerical issledo¬vanie features of supersonic flow around a circular cone with flat wings flow about. Izv. VUZov. Aviatsionnaia Tekhnika, No. 1, 53— 55 (1989) [In Russian].
14. Moore F. G., Devan L., Hymer T. New semiemperical method for computing nonlinear missile aerodynamics. J. Spacecraft and Rockets, 30 (6), 697—706 (1993).

References: V. 
 V. 
 V. 
 V. 
 V. 
 V. 
 V. 
 V. 
 V. 
 V. 
 V. 
 V. 
 V. 
 V. 
 V. 
 V. 
 V.