Heat shield cavity parametric experimental aeroheating for a proposed mars smart lander aeroshell

32nd AIAA Fluid Dynamics Conference and Exhibit

Volumn , Issue , 2002, Pages

  Liechty, Derek S ^a   Hollis, Brian R ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERO-HEATING; BOUNDARY LAYER HEIGHTS; BOUNDARY LAYER TRANSITIONS; MOMENTUM THICKNESS; NASA LANGLEY RESEARCH CENTER; NAVIER STOKES FLOW; SPACECRAFT BUS; THIN LAYERS;

AERODYNAMIC HEATING; ANGLE OF ATTACK; BOUNDARY LAYERS; CAVITY RESONATORS; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER;

HEAT SHIELDING;

EID: 84896866773     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)

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