Supersonic/hypersonic laminar heating correlations for rectangular and impact-induced open and closed cavities

46th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2008, Pages

  Everhart, Joel L ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROHEATING; BASE-LINE CONDITIONS; CAVITY GEOMETRY; CAVITY HEATING; CLOSED CAVITY; COLUMBIA ACCIDENT INVESTIGATION BOARD; CORRELATION PARAMETERS; DECAY RATE; END-WALL; ENGINEERING ASSESSMENTS; GEOMETRICAL SHAPES; GROUND BASED; LOCAL FLOW CONDITIONS; NEW CORRELATIONS; ON ORBIT; RANDOM LOCATION; RECTANGULAR GEOMETRY; SPACE SHUTTLE ORBITER; SURFACE FLOW; SURFACE HEATING; THERMAL PROTECTION SYSTEM; UNCERTAINTY BOUNDS; VEHICLE SURFACE;

AEROSPACE ENGINEERING; DAMAGE DETECTION; DECAY (ORGANIC); GEOMETRY; MANNED SPACE FLIGHT; MATHEMATICAL MODELS; SPACE DEBRIS; SPACE SHUTTLES;

HEATING;

EID: 77958498422     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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