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.
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| Format: | Others |
| Language: | English |
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North Texas State College
1957
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| Online Access: | https://digital.library.unt.edu/ark:/67531/metadc107936/ |