Simulation of flow through breach in leading edge at Mach 24

37th AIAA Thermophysics Conference

Volumn , Issue , 2004, Pages

  Gnoffo, Peter A ^a   Alter, Stephen J ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; BOUNDARY LAYERS; FLIGHT SIMULATORS;

ACCIDENT INVESTIGATION; APPROPRIATE MODELS; CAVITY GEOMETRY; EXTERNAL BOUNDARIES; EXTERNAL SHOCKS; FLIGHT CONDITIONS; GRID GENERATION; INTERNAL SURFACES;

COMPUTATIONAL FLUID DYNAMICS;

EID: 85088341885     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-2283     Document Type: Conference Paper

References (8)

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2. Cheatwood, F. M. and Gnoffo, P. A. "Users Manual for the Langley Aerothermodynamic Upwind Relaxation Algorithm (LAURA)," NASA TM 4674, April 1996.
3. Weilmuenster, K. J.; Gnoffo, P. A.; Greene, F. A., Navier-Stokes Simulations of Orbiter Aerodynamic Characteristics Including Pitch Trim and Bodyflap, Journal of Spacecraft and Rockets, Vol. 31, No. 3, May-June 1994, pp355-366.
4. Gnoffo, P. A.; Weilmuenster, K. J.; Alter, S. J., Multiblock Analysis for Shuttle Orbiter Re-entry Heating from Mach 24 to Mach 12, Journal of Spacecraft and Rockets, Vol. 31, No. 3, May-June 1994, pp367-377.
5. Kleb, W. L.; Weilmuenster, K. J., Characteristics of the Shuttle Orbiter Leeside Flow During a Re-Entry Condition, Journal of Spacecraft and Rockets, Vol. 31, No. 1, May-June 1994, pp8-16.
6. Orbiter Experiments (OEX) Aerothermodynamics Symposium, Edited by David Throckmorton, NASA Conference Publication 3248, Part I and II, April 1995.
7. Roe, P. L.: "Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes," Journal of Computational Physics, Vol.43, Oct. 1981, pp357-372.
8. Yee, H. C.: "On Symmetric and Upwind TVD Schemes," NASA TM-88325, June 1986.