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:

Published: 1948

Total Pages: 748

ISBN-13:

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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.


Report

Report

Author: United States. National Advisory Committee for Aeronautics

Publisher:

Published: 1956

Total Pages: 36

ISBN-13:

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