Computational aerothermodynamic design issues for hypersonic vehicles

Journal of Spacecraft and Rockets

Volumn 36, Issue 1, 1999, Pages 21-43

  Gnoffo, Peter A ^a,c   James Weilmuenster, K ^a,c   Harris Hamilton II, H ^a,c   Olynick, David R ^b   Venkatapathy, Ethiraj ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b NASA AMES RESEARCH CENTER   (United States)

^c Aerothermodynamics Branch   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC HEATING; HYPERSONIC AERODYNAMICS; PARAMETER ESTIMATION; REENTRY;

COMPUTATIONAL AEROTHERMODYNAMIC DESIGN; HYPERSONIC VEHICLES;

SPACECRAFT;

EID: 0032734289     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.3430     Document Type: Article

References (1)

1. Cook, S. A., "X-33 Reusable Launch Vehicle Structural Technologies," AIAA Paper 96-4573, Nov. 1996.