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A Method for Approximating the Distributed Loads of an Airplane by Sets of Point Loads

This paper gives the derivation of a method for determining the forces to be applied to these points which will simulate the load distributed over all the airplane.

Identiferoai:union.ndltd.org:unt.edu/info:ark/67531/metadc107936
Date January 1957
CreatorsAustin, Charles Wayne
ContributorsCopp, George, Cooke, J. V.
PublisherNorth Texas State College
Source SetsUniversity of North Texas
LanguageEnglish
Detected LanguageEnglish
TypeThesis or Dissertation
Formativ, 39 leaves : ill., Text
RightsPublic, Copyright, Copyright is held by the author, unless otherwise noted. All rights reserved., Austin, Charles Wayne

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