Calculations and results given serve to show how methods referred to in previous paper ("General Approach to Flutter Problem"), are applied to particular problem in flutter; calculations described for cantilever wing which was flutter tested at NACA Laboratories and test results compared with calculated results.
Use of generalized coordinates in flutter analysis
Soc Automotive Engrs -- Preprint
Society of Automotive Engineers -- Meeting ; 1943 Flutter
1943
34 pages
22 Supp sheets, Bibliography
Aufsatz (Konferenz)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Use of Generalized Coordinates in FLUTTER ANALYSIS
SAE Technical Papers | 1944
|Flutter and Divergence Analysis Using the Generalized Aeroelastic Analysis Method
Online Contents | 2008
|Flutter and Divergence Analysis Using the Generalized Aeroelastic Analysis Method
British Library Conference Proceedings | 2003
|