Span load distributions resulting from constant angle of attack, steady rolling velocity, steady pitching velocity, and constant vertical acceleration for tapered sweptback wings with streamwise tips. : Subsonic leading edges and supersonic trailing edges / Margery E. Hannah and Kenneth Margolis.
On the basis of the linearized supersonic-flow theory and theoretical spanwise distributions of circulation (which are proportional to the span load distribution) resulting from constant vertical acceleration were calculated for a series of thin, sweptback, tapered wings with streamwise tips, subson...
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| Format: | Government Document Book |
| Language: | English |
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Washington, D.C. :
National Advisory Committee for Aeronautics,
1952.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2831. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/2831
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| Y 3.N 21/5:6/2831 | Available Place a Hold |