Appraisal of Method of Flutter Analysis Based on Chosen Modes by Comparison with Experiment for Cases of Large Mass Coupling PDF Download
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Author: Donald S. Woolston
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 22
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Book Description
Results are presented for a series of flutter studies in which a Rayleigh type analysis based on chosen modes is applied to a uniform model wing carrying an arbitrarily placed concentrated weight in order to appraise the accuracy of the assumption of uncoupled modes of vibration. The results are compared with experiment.
Author: Donald S. Woolston
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 22
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Book Description
Results are presented for a series of flutter studies in which a Rayleigh type analysis based on chosen modes is applied to a uniform model wing carrying an arbitrarily placed concentrated weight in order to appraise the accuracy of the assumption of uncoupled modes of vibration. The results are compared with experiment.
Author: John L. Sewall
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 86
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Book Description
Author: John L. Sewall
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 38
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 162
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Book Description
Author: Gloria R. Champine
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 134
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 876
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Book Description
Author: John R. Spreiter
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 646
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Book Description
The aerodynamic forces and moments exerted on pitched and yawed wing-body combinations consisting of a slender body of revolution and a cruciform arrangement of thin wings have been investigated by two theoretical methods. One method, an extension of the slender wing-body theory of NACA TN No. 1662, makes possible the determination of simple closed expressions for the load distribution, of simple closed expressions for the load distribution, the forces, and the moments for slender cruciform-wing and body combinations in which the wings may be dissimilar plan form. The second method treats cruciform-wing and body combinations consisting of a body of revolution and identical wings of arbitrary aspect ratio and plan form. The results are valid at subsonic, transonic, and supersonic speeds.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1370
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Book Description
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1014
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Book Description
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1322
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Book Description
