Aerodynamics of a rectangular wing of infinite aspect ratio at high angles of attack and supersonic speeds / John C. Martin and Frank S. Malvestuto, Jr.
Perturbation of the flow over a two-dimensional flat plate at finite angles of attack is used to obtain a first-order evaluation of the damping in roll, the lift and moment due to an increment in angle of attack, and the lift and moment due to a steady pitching velocity for a rectangular wing of inf...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1955.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3421. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3421
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| Y 3.N 21/5:6/3421 | Available Place a Hold |