Experimental Investigation of an Axial-flow Supersonic Compressor Having Sharp Leading-edge Blades with an 8-percent Mean Thickness-chord Ratio PDF Download
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Author: Theodore J. Goldberg
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 38
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Book Description
Author: Theodore J. Goldberg
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 38
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 414
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 948
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Author: Robert William Fralich
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 652
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Book Description
A flutter analysis, employing slender-body aerodynamic theory and thin-plate theory, is made for rectangular wings of very low aspect ratio with a constant thickness. The spanwise variation of wing deflection is assumed to be given by a parabola, and the chordwise variation is allowed complete freedom. The results show the vsriation of flutter speed and male shape with aspect ratio. Comparisons are made with additional resuits obtained by approximating the chordwise deflection shape by use of parabolic or cubic curves. The analysis shows that the cubic approximation gives good resuits for a ratio of chord to semispan less than 3.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 716
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Author:
Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 578
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Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Industrial arts
Languages : en
Pages : 906
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 470
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