A Compilation Of Experimental Flutter Information PDF Download
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Author | : H. J. Cunningham |
Publisher | : |
Total Pages | : 34 |
Release | : 1954 |
Genre | : Flutter (Aerodynamics) |
ISBN | : |
Download A Compilation of Experimental Flutter Information Book in PDF, ePub and Kindle
Author | : Gloria R. Champine |
Publisher | : |
Total Pages | : 134 |
Release | : 1977 |
Genre | : Aeronautics |
ISBN | : |
Download A Compilation of Research Reports of Physical Research Division, Dynamic Loads Division, Loads Division, 1921 - 1973 Book in PDF, ePub and Kindle
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 500 |
Release | : 1959 |
Genre | : Aeronautics |
ISBN | : |
Download Index of NASA Technical Publications Book in PDF, ePub and Kindle
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 860 |
Release | : 1957 |
Genre | : Aeronautics |
ISBN | : |
Download Index of NACA Technical Publications Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 494 |
Release | : 1959 |
Genre | : Aeronautics |
ISBN | : |
Download Index of NASA Technical Publications Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 296 |
Release | : 1959 |
Genre | : Aeronautics |
ISBN | : |
Download A Selected Listing of NASA Scientific and Technical Reports for ... Book in PDF, ePub and Kindle
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 300 |
Release | : 1960 |
Genre | : |
ISBN | : |
Download Index to NASA Technical Publications Book in PDF, ePub and Kindle
Author | : Harry L. Runyan |
Publisher | : |
Total Pages | : 16 |
Release | : 1957 |
Genre | : Aerodynamic heating |
ISBN | : |
Download Flutter at Very High Speeds Book in PDF, ePub and Kindle
This paper is concerned with a discussion of some of the problems of flutter and aeroelasticity that are or may be important at high speeds. Various theoretical procedures for treating high Mach number flutter are reviewed. Application of two of these methods, namely, the Van Dyke method and piston-theory method, is made to a specific example and compared with linear two- and three-dimensional results. It is shown that the effects of thickness and airfoil shape are destabilizing as compared with linear theory at high Mach number. In order to demonstrate the validity of these large predicted effects, experimental flutter results are shown for two rectangular wings at Mach numbers of 6.86 and 3. The results of nonlinear piston-theory calculations were in good agreement with experiment, whereas the results of using two- and three-dimensional linear theory were not. In addition, some results demonstrating the importance of including camber modes in a flutter analysis are shown, as well as a discussion of one case of flutter due to aerodynamic heating.
Author | : |
Publisher | : |
Total Pages | : 702 |
Release | : 1957 |
Genre | : Aerodynamics |
ISBN | : |
Download NACA Conference on Aircraft Loads, Structures, and Flutter Book in PDF, ePub and Kindle
Author | : E. H. Dowell |
Publisher | : |
Total Pages | : 396 |
Release | : 1963 |
Genre | : Flutter (Aerodynamics) |
ISBN | : |
Download Experimental and Theoretical Panel Flutter Studies in the Mach Number Range of 1.0 to 5.0 Book in PDF, ePub and Kindle