AIAA-2006-1847 An Investigation of the Sensitivity of F-16 Fighter Flutter Onset and Limit Cycle Oscillations to Uncertainties
47th, AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics and materials conference ; 2006 ; Newport, R.I
2006-01-01
8 pages
Paper numbers 2006-1600 to 2006-2284 with gaps held
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Theoretical Predictions of F-16 Fighter Limit Cycle Oscillations for Flight Flutter Testing
Online Contents | 2009
|AIAA-2006-1635 Transonic Limit Cycle Flutter of High-Aspect-Ratio Swept Wings
British Library Conference Proceedings | 2006
|AIAA-2004-1694 Transonic Limit Cycle Flutter/LCO
British Library Conference Proceedings | 2004
|British Library Conference Proceedings | 2001
|