An Evaluation of Some Approximate Methods of Computing Landing Stresses in Aircraft PDF Download
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Author: Elbridge Z. Stowell
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Category :
Languages : en
Pages : 0
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Author: Elbridge Z. Stowell
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Author: Elbridge Z. Stowell
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Category : Airplanes
Languages : en
Pages : 748
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The landing of a simplified airplane structure, consisting of a uniform beam for the wings, a concentrated mass for the fuselage, and a linear spring for the landing gear, is analyzed exactly and is compared with several approximate solutions. The approximate solutions which neglect elasticity in the determination of landing-gear reaction but consider elasticity in computations of stresses give results of good accuracy and indicate that drop tests in which rigid masses are used may be a satisfactory approach to the landing problem.
Author: United States. National Advisory Committee for Aeronautics
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Category : Aeronautics
Languages : en
Pages : 1172
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Author:
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Category : Aeronautics
Languages : en
Pages : 460
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Author: United States. National Advisory Committee for Aeronautics
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Category : Aeronautics
Languages : en
Pages : 616
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Author: Albert J. Evans
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Category : Aerodynamic load
Languages : en
Pages : 326
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Author: Robert T. Yntema
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Category : Bars (Engineering)
Languages : en
Pages : 692
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A more exact mode-expansion method used in evaluating the Rayleigh approach is also described. Numerous mode shapes and derivatives obtained in conjunction with the frequency calculations are presented in tabular form.
Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category : Aeronautics
Languages : en
Pages : 1200
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Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Author:
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Category : Aeronautics
Languages : en
Pages : 1044
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Author: Society for Experimental Stress Analysis
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Category : Strains and stresses
Languages : en
Pages : 224
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