Journal of the Korea Institute of Military Science and Technology (한국군사과학기술학회지)

The Korea Institute of Military Science and Technology (한국군사과학기술학회)
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Aerodynamic Analysis of Lateral Jet Controlled Missile Using CfDS Code

CFDS 코드를 이용한 측추력 유도탄 공력해석

  • Published : 2006.06.01
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Abstract

This paper investigates effects of reaction control jet on the aerodynamic performance of generic interceptor missile operating at supersonic flight condition. Parallelized CFDS code is used as a viscous flow solver. The generic interceptor missile configuration composed of a long and slender body and fixed tail fins. The behavior of normal force, axial force and pitching moment characteristics at altitude conditions corresponding to 10 km is studied according to the given control jet conditions, different angle of attacks based on the analysis of aerodynamic characteristics.

Keywords

References

  1. Allen, H. J and Perkins, E. W. 'A Study of the Effects of Viscosity on Flow Over Slender Inclined Bodies of Revolution.' NACA Rep. 1048, 1951
  2. Qin, N., and Foster, G. W. 'Study of Flow Interactions due to a Supersonic Lateral Jet Using high Resolution Navier-Stokes Solutions', AIAA Paper 94-2151, June 1995
  3. Childs, R. E., and Caruso, S. C., 1987, 'On the Accuracy of Turbulent Base Flow Predictions', AIAA Paper No. 87-1439
  4. 홍승규, 이광섭, 'Application of Characteristic Boundary Conditions in the Flux-Difference Splitting Framework,' 대한기계학회, pp.141-156, 1999
  5. 김재관, 이정일, 김종암, 홍승규, 이광섭, 안창수, 'CFDS 코드의 효율성 개선', 춘계 한국전산유체공학회, pp.123-127, 2005
  6. Sung-soo Kim, Chongam Kim, Oh-Hyun Rho, and Seung Kyu Hong, 'Cures for the Shock Instability ; Development of Shock-Stable Roe Scheme', Journal of Computational Physics, Vol. 185(2), pp.342 - 374, 2003 https://doi.org/10.1016/S0021-9991(02)00037-2
  7. K. H. Kim, C. Kim, and O. H. Rho, 'Methods for the Accurate Computations of Hypersonic Flows, Part I : AUSMPW+ Scheme', J. of Computational Physics, Vol. 174, pp.38-80, 2001 https://doi.org/10.1006/jcph.2001.6873
  8. Wilcox, D. C., 'Turbulence Modeling for CFD', DCW Industries, Inc., 5354 Palm Drive, La Canada, Calif., 1993
  9. 김창성. '2-방정식 난류모델이 결합된 Navier-Stokes 방정식의 해석 및 응용', 서울대학교 공학박사논문, pp.85-92, 2001
  10. 이보성, 김태윤, 박영회, 이동호, '${\sigma}-SST$ 난류 모델을 적용한 벽면 근처 정사각주 유동장의 수치 해석', 한국항공우주학회지, 제31권 제8호, 2003
  11. http://www.grc.nasa.gov/ WWW/ wind/ valid/ m6wing/ m6wing.htm
  12. 이동호, 노오현, 김종암, 'CFD 유동 해석의 응용성 확대 - 2단계 최종보고서', 국방과학연구소, 2005