Aero-thermoelastic behaviour of panel substructures subjected to rapid accelerations in supersonic flow

7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization

Volumn , Issue , 1998, Pages 1011-1018

  Udrescu, Radu ^a  

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

Author keywords

[No Author keywords available]

Indexed keywords

DEGREES OF FREEDOM (MECHANICS); MACH NUMBER; SUPERSONIC FLOW; TOPOLOGY;

AEROELASTIC STABILITY; DETERMINISTIC SYSTEMS; DYNAMIC PRESSURE CHANGES; NON-LINEAR FINITE ELEMENT MODEL; NONLINEAR PANEL FLUTTER; PANEL SUBSTRUCTURE; STEADY-STATE VALUES; TRIANGULAR PLATE ELEMENTS;

AEROELASTICITY;

EID: 84982318019     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-4838     Document Type: Conference Paper

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