An Evalution Of Some Approximate Methods Of Computing Landing Stresses In Aircraft PDF Download

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An Evalution of Some Approximate Methods of Computing Landing Stresses in Aircraft

An Evalution of Some Approximate Methods of Computing Landing Stresses in Aircraft
Author: Elbridge Z. Stowell
Publisher:
Total Pages: 748
Release: 1948
Genre: Airplanes
ISBN:

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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.


Technical Note

Technical Note
Author:
Publisher:
Total Pages: 460
Release: 1950
Genre: Aeronautics
ISBN:

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Index of NACA Technical Publications

Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 616
Release: 1949
Genre: Aeronautics
ISBN:

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Annual Report of the National Advisory Committee for Aeronautics

Annual Report of the National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 1200
Release: 1954
Genre: Aeronautics
ISBN:

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Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.


Simplified Procedures and Charts for the Rapid Estimation of Bending Frequencies of Rotating Beams

Simplified Procedures and Charts for the Rapid Estimation of Bending Frequencies of Rotating Beams
Author: Robert T. Yntema
Publisher:
Total Pages: 692
Release: 1955
Genre: Bars (Engineering)
ISBN:

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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.