Theoretical lift and damping in roll of thin wings with arbitrary sweep and taper at supersonic speeds. : Supersonic leading and trailing edges / Sidney M. Harmon and Isabella Jeffreys.
Generalized expressions are obtained by means of the linearized theory of the surface velocity potential, the surface-pressure distribution, the lift due to angle of attack, and the rolling moment due to steady rolling motion for a series of thin tapered and swept wings. The results are applicable t...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1950.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2114. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/2114
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| Y 3.N 21/5:6/2114 | Available Place a Hold |