Risk mitigation study for instrumentation layout along wing leading edge of a 1.8%-scale space shuttle model using TSP

43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers

Volumn , Issue , 2005, Pages 12819-12851

  Smolinski, Gregory J ^a,c,d   Huhner, James P ^b,d,e,f   Holden, Michael S ^a,c,d  

^a CUBRC   (United States)

^b UNIVERSITY OF FLORIDA   (United States)

^c Aerothermal Aero Optics Evaluation Center   (United States)

^d AIAA   (United States)

^e Department of Aerospace Engineering Mechanics and Engineering Science

^f AIAA Ground Testing Technical Committee

Author keywords

[No Author keywords available]

Indexed keywords

DATA SETS; RISK MITIGATION; SHOCK TUNNELS; THIN-FILM GAUGES;

HEAT TRANSFER; HEATING; MATHEMATICAL MODELS; RISK MANAGEMENT; SHOCK TUBES; THIN FILMS; WINGS;

SPACE SHUTTLES;

EID: 30744434641     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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