An Experimental Investigation of Aerodynamic Effects of Airfoil Thickness on Transonic Flutter Characteristics PDF Download
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Author: Robert V. Doggett
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 28
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Author: Robert V. Doggett
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 28
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Book Description
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1014
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Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 2300
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 858
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 836
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 818
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Author: Perry W. Hanson
Publisher:
ISBN:
Category : Aeroelasticity
Languages : en
Pages : 56
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Book Description
Results of flutter tests on some simple all-movable-control-type models are given. One set on models, which had a square planform with double-wedge airfoils with four different values of leading- and trailing-edge radii from 0 to 6 percent chord and airfoil thickness of 9, 11, 14, and 20 percent chord, was tested at Mach numbers from 0.7 to 6.86. The bending-to-torsion frequency ratio was about 0.33. The other set of models, which had a tapered planform with single-wedge and double-wedge airfoils with thickness of 3, 6, 9, and 12 percent chord, was tested at Mach numbers from 0.7 to 3.98 and a frequency ratio of about 0.42.
Author:
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ISBN:
Category : Aerodynamics
Languages : en
Pages : 652
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Author:
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ISBN:
Category : Government publications
Languages : en
Pages : 1086
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Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1878
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