AIAA-2004-1696 Modeling Limit Cycle Oscillation Behavior of the F-16 Fighter Using a Harmonic Balance Approach
45TH, Structures, structural dynamics, and materials conference:; 45th AIAA/ASME/ASCE/AHS/ASC 12th AIAA/ASME/AHS adaptive structures conference: 6th AIAA non-deterministic approaches forum: 5th AIAA gossamer spacecraft forum ; 2004 ; Palm Springs, Calif
2004-01-01
7 pages
Held in conjunction with 12th AIAA/ASME/AHS adaptive structures conference, 6th AIAA non-deterministic approaches forum and 5th AIAA gossamer spacecraft forum
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Modeling Viscous Transonic Limit Cycle Oscillation Behavior Using a Harmonic Balance Approach
British Library Conference Proceedings | 2002
|Modeling Viscous Transonic Limit-Cycle Oscillation Behavior Using a Harmonic Balance Approach
Online Contents | 2004
|