Effect of isolated roughness elements on boundary-layer transition for Shuttle Orbiter

Journal of Spacecraft and Rockets

Volumn 34, Issue 4, 1997, Pages 426-436

  Bertin, John J ^a,e   Stetson, Kenneth F ^b,e   Bouslog, Stanley A ^c,e   Caram, Jose M ^d,e  

^a UNITED STATES AIR FORCE ACADEMY   (United States)

^b Rohr Industries Inc ^*

^c GOODRICH CORPORATION   (United States)

^d NASA JOHNSON SPACE CENTER   (United States)

^e AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

HEAT FLUX; HEAT TRANSFER; SPACE SHUTTLES; SURFACE ROUGHNESS; TEMPERATURE MEASURING INSTRUMENTS; TRANSITION FLOW; WIND TUNNELS;

MACH NUMBER; SPACE SHUTTLE ORBITER;

BOUNDARY LAYER FLOW;

EID: 0031188570     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.3254     Document Type: Article

References (13)

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