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Stress analysis of door and window of a passenger aircraft

Published online by Cambridge University Press:  04 July 2016

V. G. Ukadgaonker
Affiliation:
Department of Mechanical Engineering, Indian Institute of Technology, Bombay, Powai, Mumbai, India
P. J. Awasare
Affiliation:
Department of Mechanical Engineering, Indian Institute of Technology, Bombay, Powai, Mumbai, India
S. V. Gade
Affiliation:
Department of Mechanical Engineering, Indian Institute of Technology, Bombay, Powai, Mumbai, India

Abstract

The stresses around the passenger door, emergency door and window of an aircraft, Airbus A300B, are considered in this paper. By idealising these opening as rectangular holes with rounded corners in an infinite plate subjected to inplane loads and considering the presence of adjacent holes the stresses are determined using the complex variable method along with Schwarz Alternating Method. The results of the analytical solution are found to be in good agreement with those of the finite element analysis using ANSYS 5.0 software within 5%.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1979 

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References

1. Muskhelishvili, N.I. Some Basic Problems of Mathematical Theory of Elasticity, P. Noordhoff, Netherlands, Third Edition, 1953.Google Scholar
2. Savin, G.N., Stress Concentration Around Holes, Pergamon Press, London, 1961.Google Scholar
3. Wittrick, W.H. Some simple transformation functions for square and triangular holes with rounded corners, Aeronaut Q, May 1960, 11, pp 195199.Google Scholar
4. Sokolnikoff, I.S. Mathematical Theory of Elasticity, McGraw Hill Book Company, New York, 1956.Google Scholar
5. Ukadgaonker, V.G. Stress analysis of plate with two unequal circular holes subjected to tangential stresses, AIAA J, January 1980, 18, (1), pp 125128.Google Scholar
6. Ukadgaonker, V.G. and Patil, D.B. Stress analysis of a plate con taining two elliptical holes subjected to uniform pressure and Tan gential stresses at the hole boundaries, Trans of ASME, J of Eng for Industry, February 1993, 115, pp 93101.Google Scholar
7. Airbus Industries, Engineering Notes: A300B Aircraft, 1979, Versailles, France.Google Scholar
8. Gade, S.V. Stress Analysis of the Door and Window of a Passenger Aircraft,MTech dissertation, 11T, Bombay, 1993.Google Scholar
9. Awasare, P.J. Some Closed Form Solutions in Two Dimensional Elasticity and Fracture Mechanics,PhD Thesis, IIT Bombay, 1995.Google Scholar