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Elastic and Equilibrium Matrices of General Semi-Monocoque Membrane Elements

Published online by Cambridge University Press:  04 July 2016

J. Robinson ,
R. Williams  and
G. W. Haggenmacher
J. Robinson
Affiliation:
Lockheed-California Company
R. Williams
Affiliation:
Lockheed-California Company
G. W. Haggenmacher
Affiliation:
Lockheed-California Company
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Extract

Many structures are made up of skin material which is stiffened by reinforcing members. Configurations of this type are predominant in the aircraft industry where they are referred to as semi-monocoque structures. When analysing such structures, using finite element techniques, the reinforcing members (stringers) are lumped together to form pure axial elements and the skin is then represented by isotropic plane stress elements.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 74 , Issue 714 , June 1970 , pp. 502 - 506
Copyright
Copyright © Royal Aeronautical Society 1970 

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References

1. Morley, L. S. D. Skew Plates and Structures. Pergamon Press Ltd, London, 1963.Google Scholar
2. Robinson, J. Structural Matrix Analysis for the Engineer. John Wiley and Sons, Publishers, New York, 1966.Google Scholar
3. Robinson, J. and Haggenmacher, G. W. Transformation of Variables for Redundancy Optimisation in the Rank Force Method. Paper presented at the 10h ASME/A1AA Structures, Structural Dynamics and Materials Conference, New Orleans, La, USA, April 1969.Google Scholar