Lift and pitching moment at supersonic speeds due to constant vertical acceleration for thin sweptback tapered wings with streamwise tips. : Supersonic leading and trailing edges / Isabella J. Cole and Kenneth Margolis.
On the basis of a solution to the linearized time-dependent wave equation, the nondimensional lift derivative and corresponding pitching-moment derivative resulting from constant vertical acceleration (that is, linear variation of angle of attack with time) are evaluated for a family of thin sweptba...
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| Format: | Government Document Book |
| Language: | English |
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Washington, D.C. :
National Advisory Committee for Aeronautics,
1954.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3196. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3196
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| Y 3.N 21/5:6/3196 | Available Place a Hold |