Impact of fluid-thermal-structural coupling on response prediction of hypersonic skin panels

AIAA Journal

Volumn 49, Issue 11, 2011, Pages 2393-2406

  Culler, Adam J ^a   McNamara, Jack J ^b,c  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b OHIO STATE UNIVERSITY   (United States)

^c AFRL/RBSM Structural Sciences Center ^*  (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC HEATING; AERODYNAMICS; CARBON; DEFORMATION; SPACE PLATFORMS; THERMAL EXPANSION;

IN-PLANE BOUNDARY CONDITIONS; PREDICTIVE CAPABILITIES; QUASI STATIC RESPONSE; RESPONSE PREDICTION; STRUCTURAL DEFORMATION; STRUCTURAL INTERACTIONS; THERMAL-STRUCTURAL COUPLING; UNITED STATES AIR FORCE;

FORECASTING;

EID: 80055059100     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.J050617     Document Type: Article

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