Aeroelastic analysis for future air vehicle concepts using a fully nonlinear methodology

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

Volumn 7, Issue , 2005, Pages 4575-4608

  Strganac, Thomas W ^a,c   Cizmas, Paul G ^a,c   Nichkawde, Chetan ^a,c   Gargoloff, Joaquin ^a,c   Beran, Philip S ^b,c  

^a TEXAS A AND M UNIVERSITY   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; AIRCRAFT PARTS AND EQUIPMENT; BOUNDARY LAYERS; DYNAMICS; METHOD OF MOMENTS; SYSTEMS SCIENCE; TRANSONIC AERODYNAMICS;

AEROELASTIC ANALYSIS; AIR VEHICLES; HIGH-FIDELITY MODELING; NONLINEAR ANALYSIS;

AERODYNAMICS;

EID: 28844456103     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-2171     Document Type: Conference Paper

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