Art

J-GLOBAL ID：200902270403328307   Reference number：09A0531086

Flutter Prediction Using Continuous Wavelet Transform

連続ウェーブレット変換を使用したフラッタ予測

Author (3)： UEDA Tetsuhiko (Dep. of Aerospace Engineering, Nagoya Univ.) ,  IIO Masanobu (Dep. of Aerospace Engineering, Nagoya Univ.) ,  IKEDA Tadashige (Dep. of Aerospace Engineering, Nagoya Univ.)
Material： Transactions of the Japan Society for Aeronautical and Space Sciences  (Trans Jpn Soc Aeronaut Space Sci)
Volume： 51  Issue： 174  Page： 275-281 (J-STAGE)  Publication year： 2009 
JST Material Number： F0167A  ISSN： 0549-3811  CODEN： TJASA  Document type： Article
Article type： 原著論文  Country of issue： Japan (JPN)  Language： ENGLISH (EN)

Thesaurus term： *wavelet transform ,  extrapolation method ,  *flutter ,  low speed wind tunnel ,  measurement data ,  *wind tunnel test ,  aspect ratio ,  *blade(machine element) ,  prediction technique

JST classification (1)： Aerodynamics of aircrafts  (QK02010T)

Reference (7)：

• LIND, R. Flight-Test Evaluation of Flutter Prediction Methods. J. Aircraft. 2003, 40, 964-970
• CHUI, C. K. An Introduction to Wavelets. 1992
• KOORNWINDER, T. H. ed. WAVELETS : An Elementary Treatment of Theory and Applications. 1993
• COLE, H. A. Jr. On-Line Failure Detection and Damping Measurement of Aerospace Structures by Random Decrement Signatures. 1973
• BRIGNAC, W. J. The Random Decrement Technique Applied to the YF-16 Flight Flutter Tests. ASME, and SAE, Structures Structural Dynamics, and Materials Conference, 16th, Denver, Colo., 1975. 1975

Terms in the title (3)： 連続ウェーブレット変換 ,  フラッタ ,  予測