Author: M. H. Lock
Publisher:
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).
Comparative Experimental and Theoretical Studies of the Flutter of Flat Panels in a Low Supersonic Flow
Author: M. H. Lock
Publisher:
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).
Publisher:
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).
Experimental and Theoretical Panel Flutter Studies in the Mach Number Range of 1.0 to 5.0
Author: E. H. Dowell
Publisher:
ISBN:
Category : Flutter (Aerodynamics)
Languages : en
Pages : 396
Book Description
Publisher:
ISBN:
Category : Flutter (Aerodynamics)
Languages : en
Pages : 396
Book Description
NASA Technical Note
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 536
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 536
Book Description
Theoretical Flutter Analysis of Flat Rectangular Panels in Uniform Coplanar Flow with Arbitrary Direction
Author: Eldon Eugene Kordes
Publisher:
ISBN:
Category : Gas flow
Languages : en
Pages : 22
Book Description
Publisher:
ISBN:
Category : Gas flow
Languages : en
Pages : 22
Book Description
Report
Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Publisher:
ISBN:
Category :
Languages : en
Pages : 716
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 716
Book Description
Monthly Catalog of United States Government Publications
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1464
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1464
Book Description
Report
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 330
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 330
Book Description
Further Experimental Results on the Influence of the Turbulent Boundary Layer on Panel Flutter
Author: Peter A. Gaspers (Jr.)
Publisher:
ISBN:
Category : Flutter (Aerodynamics)
Languages : en
Pages : 52
Book Description
Turbulent boundary layer effects on flutter of flat rectangular panels.
Publisher:
ISBN:
Category : Flutter (Aerodynamics)
Languages : en
Pages : 52
Book Description
Turbulent boundary layer effects on flutter of flat rectangular panels.
Bibliography of Scientific and Industrial Reports
Author:
Publisher:
ISBN:
Category : Research
Languages : en
Pages : 1352
Book Description
Publisher:
ISBN:
Category : Research
Languages : en
Pages : 1352
Book Description
Structural Dynamics of High Speed Flight
Author:
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 778
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 778
Book Description