Analysis of flows over a SST wing-body configuration at low speed and high angles of attack

21st AIAA Applied Aerodynamics Conference

Volumn , Issue , 2003, Pages

  Lei, Zhong ^a   Kwak, Dong Youn ^b   Noguchi, Masayoshi ^b   Iwamiya, Toshiyuki ^b  

^a Project Development Department   (Japan)

^b JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; FLOW FIELDS; NAVIER STOKES EQUATIONS; SUPERSONIC AIRCRAFT;

AERODYNAMIC CHARACTERISTICS; COMPUTATIONAL RESULTS; HIGH ANGLES OF ATTACK; NUMERICAL COMPUTATIONS; SURFACE FLOW PATTERNS; WIND TUNNEL EXPERIMENT; WIND TUNNEL MODELING; WING-BODY CONFIGURATIONS;

WIND TUNNELS;

EID: 85067322273     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-3415     Document Type: Conference Paper

References (10)

1. Brennenstuhl, U. & Hummel, D., "Vortex Formation over Double-Delta Wings", ICAS-82-6.6.3.
2. Verhaagen, N.G., Jenkins, L.N., Kern, S.B. and Washburn, A.E., "A Study of the Vortex Flow over a 76/40-deg Double-Delta Wing," AIAA paper 95-0650.
3. Gortz, S. and Rizzi, A., "Computing the High-Alpha Aerodynamics of Delta Wings Evaluation and Analysis," AIAA paper 2001-0015.
4. Ericcson, L., "Further Analysis of Fuselage Effects on Delta Wing," AIAA paper 2000-0981.
5. Rogers, S. and Roth, K., "Validation of Computed High-Lift Flows with Significant Wind-Tunnel Effects" AIAA Journal, Vol.39, No.10, Oct. 2001, pp.1884-1892.
6. Verhaagen, N.G., "Tunnel Wall Effect on the Flow around a 76/40-deg Double-Delta Wing," AIAA paper 98-0312.
7. Sakata, K., "Supersonic Research Program in NAL, Japan", International CFD Workshop for Super-Sonic Transport Design, 1998, pp.1-4
8. Yoshida, K.: "Aerodynamic Design Technology of Scaled Supersonic Experiment Airplane," Proceedings of 2001 Meeting of Japan Society of Fluid Mechanics, 2001, pp.547-548 (in Japanese).
9. Kwak, D., Miyata, K., Noguchi, M., Sunada, Y. and Ronoie, K., "Experimental Investigation of High Lift Device for SST," NAL TR-1450, 2002, National Aerospace Laboratory of Japan.
10. Watanabe, S. and Kato, H., "Stereo PIV Applications to Large-Scale Low-Speed Wind Tunnels," AIAA paper 2003-919. 11. Theodorsen, T. and Silverstein, "Experimental Verification of the Theory of Wind-Tunnel Interference," NACA Report 478, 1933.