Theory of aircraft structural models subject to aerodynamic heating and external loads / William J. O'Sullivan, Jr.
The problem of investigating the simultaneous effects of transient aerodynamic heating and external loads on aircraft structures for the purpose of determining the ability of the structure to withstand flight to supersonic speeds is studied. By dimensional analyses it is shown that.
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington :
National Advisory Committee for Aeronautics,
[1957]
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
4115. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/4115
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| Y 3.N 21/5:6/4115 | Available Place a Hold |