An Evaluation of Some Approximate Methods of Computing Landing Stresses in Aircraft PDF Download

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

An Evaluation of Some Approximate Methods of Computing Landing Stresses in Aircraft PDF Author: Elbridge Z. Stowell
Publisher:
ISBN:
Category :
Languages : en
Pages : 0

Book Description


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

An Evaluation of Some Approximate Methods of Computing Landing Stresses in Aircraft PDF Author: Elbridge Z. Stowell
Publisher:
ISBN:
Category :
Languages : en
Pages : 0

Book Description


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

An Evalution of Some Approximate Methods of Computing Landing Stresses in Aircraft PDF Author: Elbridge Z. Stowell
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 748

Book Description
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 - National Advisory Committee for Aeronautics

Technical Note - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1172

Book Description


Technical Note

Technical Note PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 460

Book Description


A Comparison of the Experimental Subsonic Pressure Distributions about Several Bodies of Revolution with Pressure Distributions Computed by Means of the Linearized Theory

A Comparison of the Experimental Subsonic Pressure Distributions about Several Bodies of Revolution with Pressure Distributions Computed by Means of the Linearized Theory PDF Author: Albert J. Evans
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 326

Book Description


Index of NACA Technical Publications

Index of NACA Technical Publications PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 616

Book Description


Report - National Advisory Committee for Aeronautics

Report - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 664

Book Description


Annual Report of the National Advisory Committee for Aeronautics

Annual Report of the National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1200

Book Description
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 PDF Author: Robert T. Yntema
Publisher:
ISBN:
Category : Bars (Engineering)
Languages : en
Pages : 692

Book Description
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.

Aeronautical Engineering Review

Aeronautical Engineering Review PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 2126

Book Description