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Stresses and Deflection in a Flat Plate with Clamped Edges under Normal Pressure

Published online by Cambridge University Press:  28 July 2016

J. K. Oaks
J. K. Oaks*
Affiliation:
Royal Aircraft Establishment
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Extract

Tests were made at the request of the Royal Aeronautical Society Structures Committee to extend the information on Data Sheet 02.09.02 from a value of the parameter.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 57 , Issue 508 , April 1953 , pp. 244 - 246
Copyright
Copyright © Royal Aeronautical Society 1953

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