Author: L. E. GoodmanPublisher:
ISBN:
Category : Elastic plates and shells
Languages : en
Pages : 92
Book Description
Supersonic Speed Flutter Analysis of Circular Panels with Edges Elastically Restrained Against Rotation
Author: L. E. GoodmanPublisher:
ISBN:
Category : Elastic plates and shells
Languages : en
Pages : 92
Book Description
Supersonic Speed Flutter Analysis of Circular Panels with Edges Elastically Restrained Against Rotation
Author: Jasti Venkata RattayyaPublisher:
ISBN:
Category : Elastic plates and shells
Languages : en
Pages : 244
Book Description
A Review of the Air Force Materials Research and Development Program
Author: Junie J. BanksPublisher:
ISBN:
Category : Materials
Languages : en
Pages : 214
Book Description
These reports cover basic and applied research in the materials area being conducted by the Metals and Ceramics, Nonmetallic Materials, Physics, Manufacturing Technology and Applications Laboratories of the Directorate of Materials and Processes.
Comparative Experimental and Theoretical Studies of the Flutter of Flat Panels in a Low Supersonic Flow
Author: M. H. LockPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 180
Book Description
A series of panel flutter experiments were performed in the GALCIT transonic wind tunnel. The preflutter panel motion and the motion during flutter were studied in detail. Flutter boundaries were obtained between Mach numbers 1.15 and 1.5. Three analytical studies of the flutter phenomenon, based upon conventional assumptions, are presented which facilitate comparison between theory and experiment. A detailed comparison between the theoretical and experimental results reveals considerable disagreement in the flutter boundaries at supersonic Mach numbers less than 1.4. The agreement between theory and experiment improves at the higher Mach numbers. The theory appears inadequate for the prediction of flutter boundaries at the lower supersonic Mach numbers. A possible cause of this inadequacy of the theory is discussed. (Author).
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