Coupled flow-thermal-structural analysis for response prediction of hypersonic vehicle skin panels

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn , Issue , 2010, Pages

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

^a The Ohio State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

A-CARBON; COMMERCIAL SOFTWARE; COMPUTATIONAL EXPENSE; COUPLED FLOW; ELEVATED STRESS; EXTREME ENVIRONMENT; FAILURE INDEX; FLUCTUATING PRESSURES; HEATING ANALYSIS; HIGHER MODE; HYPERSONIC FLIGHTS; IN-PLANE; KEY CHARACTERISTICS; MULTISCALES; MUTUAL COUPLING; NON-UNIFORM SKIN; PEAK DISPLACEMENT; PREDICTION CAPABILITY; QUASI-STATIC; QUASI-STATIC STRUCTURAL RESPONSE; RESPONSE PREDICTION; SKIN TEMPERATURES; SNAP-THROUGH; STRUCTURAL DEFORMATION; STRUCTURAL INTERACTIONS; STRUCTURAL SOLUTIONS; SURFACE PRESSURES; TEMPORAL COUPLING; THERMAL-STRUCTURAL ANALYSIS; TRANSIENT DYNAMICS; UNITED STATES AIR FORCE;

AERODYNAMIC HEATING; BOUNDARY CONDITIONS; DEFORMATION; DYNAMIC RESPONSE; ECOLOGY; FORECASTING; HYPERSONIC AERODYNAMICS; HYPERSONIC VEHICLES; SPACE PLATFORMS; STRUCTURAL DYNAMICS; SURFACES; THERMODYNAMICS;

THERMAL EXPANSION;

EID: 84855625136     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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