Aeroelastic analysis of F-16 and F-18/A configurations using adapted CFD-based reduced-order models

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

Volumn 8, Issue , 2007, Pages 7943-7962

  Amsallem, David ^a,b   Farhat, Charbel ^a,c,d   Lieu, Thuan ^a,c  

^a STANFORD UNIVERSITY   (United States)

^b Department of Aeronautics and Astronautics Department of Mechanical Engineering and Industrial for Computational and Mathematical Engineering   (United States)

^c Stanford University   (United States)

^d AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTIC SIMULATIONS; ALTERNATIVE ROM ADAPTATION METHODS; REDUCED ORDER MODELS (ROM);

ANGLE MEASUREMENT; COMPUTATIONAL FLUID DYNAMICS; CORRELATION METHODS; INTERPOLATION; MACH NUMBER; ROBUST CONTROL;

AERODYNAMICS;

EID: 34547513959     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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