Enhanced aeroelastic analysis of panels under transitory hypersonic flow conditions

AIAA journal

Volumn 38, Issue 5, 2000, Pages 755-761

  Udrescu, Radu ^a   Surace, Giuseppe ^b  

^a National Research and Development Institute for Gas Turbines COMOTI   (Romania)

^b POLITECNICO DI TORINO   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE VEHICLES; AIRCRAFT PARTS AND EQUIPMENT; BUCKLING; COMPUTATIONAL FLUID DYNAMICS; FINITE ELEMENT METHOD; MATHEMATICAL MODELS; MATRIX ALGEBRA; REENTRY; THERMAL STRESS; THERMOELASTICITY; TRANSITION FLOW;

AEROELASTIC STABILITY; AEROTHERMOELASTIC MODEL; STABILITY MAP;

HYPERSONIC AERODYNAMICS;

EID: 0034188368     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1046     Document Type: Article

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