A reduced-order modeling framework for integrated thermo-elastic analysis of hypersonic vehicles

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

Volumn , Issue , 2009, Pages

  Falkiewicz, Nathan J ^a   Cesnik, Carlos E S ^a  

^a UNIVERSITY OF MICHIGAN   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AVIATION; CONTROL SURFACES; CONTROL SYSTEM SYNTHESIS; DESIGN AIDS; ELASTIC MODULI; EQUATIONS OF MOTION; FLIGHT CONTROL SYSTEMS; FLIGHT DYNAMICS; HEAT TRANSFER; HYPERSONIC AERODYNAMICS; PRINCIPAL COMPONENT ANALYSIS; STIFFNESS MATRIX; STRUCTURAL ANALYSIS; STRUCTURAL DYNAMICS; THERMOELASTICITY;

COMPUTATIONALLY EFFICIENT; GEOMETRIC STIFFNESS MATRIX; PROPER ORTHOGONAL DECOMPOSITIONS; REDUCED ORDER MODELS; TEMPERATURE-DEPENDENT YOUNG'S MODULUS; THERMAL BOUNDARY CONDITIONS; THERMOELASTIC ANALYSIS; TRANSIENT HEAT TRANSFER;

HYPERSONIC VEHICLES;

EID: 84855617893     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-2308     Document Type: Conference Paper

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