AIAA-2006-2132 Flutter Boundary Prediction of Smart Wings During Adaptation Using Steady Response Data
47th, AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics and materials conference ; 2006 ; Newport, R.I
2006-01-01
7 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.
DataCite | 1886
AIAA-2006-1635 Transonic Limit Cycle Flutter of High-Aspect-Ratio Swept Wings
British Library Conference Proceedings | 2006
|Flutter Boundary Prediction of Digitalized Smart Multimode Systems Using Steady-State Responses
British Library Conference Proceedings | 2009
|