Aerodynamic Loading Characteristics Including Effects of Aeroelasticity of Thin-trapezoidal-wing-body Combination at Mach Number of 1.43 [with List of References] PDF Download
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![Aerodynamic Loading Characteristics Including Effects of Aeroelasticity of Thin-trapezoidal-wing-body Combination at Mach Number of 1.43 [with List of References] PDF](https://books.google.com/books/content/images/frontcover/8I4AtAEACAAJ?fife=w150-h200)
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Languages : en
Pages : 39
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![Aerodynamic Loading Characteristics Including Effects of Aeroelasticity of Thin-trapezoidal-wing-body Combination at Mach Number of 1.43 [with List of References] PDF](https://books.google.com/books/content/images/frontcover/8I4AtAEACAAJ?fife=w80-h100)
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Languages : en
Pages : 39
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Author:
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Category :
Languages : en
Pages : 44
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Author: Harold L. Robinson
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ISBN:
Category : Aerodynamic load
Languages : en
Pages : 94
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Author: John L. Crigler
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ISBN:
Category : Aerodynamic load
Languages : en
Pages : 38
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Author: Harry W. Carlson
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Category :
Languages : en
Pages : 20
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Author: Franklin W. Diederich
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ISBN:
Category : Aerodynamic load
Languages : en
Pages : 110
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Charts are presented for the estimation of aeroelastic effects on spanwise lift distribution, lift-curve slope, aerodynamic career, and damping in roll of swept and unswept wings at subsonic and supersonic speeds. Some design considerations brought out by the results of this paper are discussed.
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Category :
Languages : en
Pages : 32
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Author: Richard E. Kuhn
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Category : Aerodynamic load
Languages : en
Pages : 50
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Author: Charlie M. Jackson
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ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 44
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This report describes a theoretical method for estimating the aerodynamic loading on a wing-body configuration. In order to provide a basis for evaluation of the method, experimental measurements of surface pressures, forces, and moments were made on a series of basic wing-body configurations over a Mach number range from 2.5 to 4.5. Comparison of the theoretical estimates with these experimental data generally indicated good agreement for the entire range of configurations and test conditions.
![Calculation of Aerodynamic Loading and Twist Characteristics of Flexible Wing at Mach Numbers Approaching 1.0 and Comparison with Experiment [with List of References] PDF](https://books.google.com/books/content/images/frontcover/niV4swEACAAJ?fife=w80-h100)
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Category : Airplanes
Languages : en
Pages : 17
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