Effect of sidewall configurations on the aerodynamic performance of supersonic air-intake

38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2002, Pages

  Watanabe, Y ^a   Murakami, A ^a   Fujiwara, H ^a  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

AERO-DYNAMIC PERFORMANCE; PRESSURE RECOVERY; SEPARATION VORTEX; SPATIAL DISTORTION; WIND TUNNEL TESTS;

COMPUTER SIMULATION; NUMERICAL MODELS; PROPULSION; WIND STRESS;

AERODYNAMIC CONFIGURATIONS;

EID: 84896693157     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. Seddon, J. and Goldsmith, E. L., "Intake Aerodynamics, " AIAA Education Series ISBN 0-93040-03-7, 1985.
2. Myong, H. K. and Kasagi, N., "A new approach to the improvement of k-epsilon turbulence model for wall-bounded shear flow, " JSME International Journal of Fluid Engineering, Vol. 109, 1990, pp. 156-160.
3. Roe, P. L., "Approximates Riemann Solvers, Parameter Vectors and Difference Schemes, " Journal of Computational Physics, Vol. 43, 1981, pp. 357-372.
4. Chakravarthy, S. R. and Osher, S., "A new class of high accuracy TVD schemes for hyperbolic conservation laws, " AIAA paper 85-0243, 1985.
5. Ferri. A. and Nucci, L. M., "The origin of aerodynamic instability of supersonic inlets at subcritical conditions, " NACA, RM L50 K30, 1.
6. Fujiwara, H., Murakami, A. and Watanabe, Y., "Numerical analysis on shock oscillation of two-dimensional external compression intakes, " AIAA paper 2002-2740, 2002.