Interval Finite Element Analysis of Wing Flutter (TN)
CHINESE JOURNAL OF AERONAUTICS ; 21 , 2 ; 134-140
01.01.2008
7 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Optimization of Wing Structures for Flutter: An Interval Approach
British Library Conference Proceedings | 2008
|NTRS | 1982
|