Aeroheating testing and predictions for project Orion CEV at turbulent conditions

46th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2008, Pages

  Hollis, Brian R ^a   Berger, Karen T ^a   Horvath, Thomas J ^a   Coblish, Joseph J ^b   Norris, Joseph D ^b   Lillard, Randolph P ^c   Kirk, Benjamin S ^c  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b Arnold Engineering Development Center ^*  (United States)

^c NASA JOHNSON SPACE CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADIABATIC WALL; AEROHEATING; ARNOLD ENGINEERING DEVELOPMENT CENTER; AUGMENTATION RATIO; CENTERLINES; CREW EXPLORATION VEHICLES; DATA SETS; ENTHALPY LEVELS; EXPERIMENTAL DATA; EXPERIMENTAL UNCERTAINTY; FLIGHT VEHICLES; FREE STREAM; HEATING DISTRIBUTIONS; HYPERVELOCITY WIND TUNNEL; NASA LANGLEY RESEARCH CENTER; POINT LOCATION; SCALE MODELS; STANTON NUMBERS; TEST CONDITION; TEST GAS; TURBULENT HEATING; WIND TUNNEL TESTS;

AERODYNAMIC HEATING; AERODYNAMICS; AEROSPACE ENGINEERING; BOUNDARY LAYERS; ENTHALPY; FORECASTING; HYDRAULICS; NASA; NOZZLES; PLANETS; REYNOLDS NUMBER; THERMOCOUPLES; UNCERTAINTY ANALYSIS; WIND TUNNELS;

ATMOSPHERIC THERMODYNAMICS;

EID: 77958456737     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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