Analysis of the scaling effects for missile configuration with lateral thruster

37th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1999, Pages

  Hsieh, Tsuying ^a  

^a NAVAL SURFACE WARFARE CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; FLUID DYNAMICS; FREE FLIGHT; HULLS (SHIP); MISSILES; REYNOLDS NUMBER; WIND TUNNELS;

COMPUTATIONAL GRIDS; EMPIRICAL SCALING; FLIGHT CONDITIONS; MISSILE CONFIGURATION; NORMAL FORCE COEFFICIENTS; PITCHING MOMENT COEFFICIENTS; THRUST COEFFICIENTS; WIND TUNNEL MODELING;

COMPUTATIONAL FLUID DYNAMICS;

EID: 84983190592     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. Praharaj, S. C., Roger, R. P., Chan, S. C, and Brooks, W. B., "CFD Computations to Scale Jet Interaction Effects from Tunnel to Flight" AIAA Paper 97-0406, Jan 1997.
2. Roger, R. P., Private communication.
3. User Manual, GASP Version 3-The General Aerodynamic Simulation Program, Aerosoft, Inc., 1872 Pratt Dr., Suite 1275, Blacksburg, VA 24060-6363, May 1996.
4. Hsieh, T., Priolo, F. J., Wardlaw, A. B. Jr. and Van Dyken, R., "Navier Stokes Calculation of Flow Over a Complete Missile to 60 Degree Incidence" AIAA Paper 95-0760, Jan 1995
5. Hsieh, T. and Wardlaw, A. B. Jr., "Numerical Simulation of Cross Jets in Hypersonic Flow Over a Biconic Body" AIAA Papa 94-0165, Jan 1994.
6. Thomas, J. L., Taylor S. L. and Anderson, W. K., "Navier Stokes Computations of Vortical Flows Over Low Aspect Ratio Wings" AIAA Paper 87-0207, Jan 1987.
7. Hsieh T., "GASP Analysis of the Scaling Effects for the AIT Configuration with Lateral Thruster at 110 kf and Mach 8" unpublished report to Ballistic Missile Defense Organization, September 1998.
8. Kao, D. L. and Shen, H W., "Numerical Surface Flow Visualization" AIAA Paper 98-0076, Jan 1998.