Single-degree-of-freedom-flutter Calculations for a Wing in Subsonic Potential Flow and Comparison with an Experiment PDF Download
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Author: Harry L. Runyan
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 36
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Book Description
The effect of Mach number and structural damping on single-degree-of-freedom pitching of a wing is presented in this report. Some experimental results are compared with theory and good agreement is found for certain ranges of an inertia parameter.
Author: Harry L. Runyan
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 36
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Book Description
The effect of Mach number and structural damping on single-degree-of-freedom pitching of a wing is presented in this report. Some experimental results are compared with theory and good agreement is found for certain ranges of an inertia parameter.
Author: Arthur W. Goldstein
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 236
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 30
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1208
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1200
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Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1308
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Book Description
Author: Horace John Grover
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 716
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Book Description
This report presents of axial-load fatigue tests on notched specimens of 24S-T3 and 75S-T6 aluminum alloys and normalized SAE 4130 steel with stress-concentration factors of 2.0 (central-circular hole, symmetrical edge notches, and fillets) and 4.0 (symmetrical edge notches and fillets). Fatigue tests were run at several levels of nominal mean stress. Results are compared with previous data for unnotched specimens.
Author: Y C Fung
Publisher: Courier Dover Publications
ISBN: 0486469360
Category : Technology & Engineering
Languages : en
Pages : 516
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Book Description
Geared toward advanced undergraduates and graduate students, this outstanding text surveys aeroelastic problems, their historical background, basic physical concepts, and the principles of analysis.
Author: A. J. Eggers
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 286
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 750
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Book Description
