Effect of tail surfaces on the base drag of a body of revolution at Mach numbers of 1.5 and 2.0 / J. Richard Spahr and Robert R. Dickey.
A wind-tunnel investigation was made of the effect of rectangular plan-form tail surfaces on the base drag of an unboattailed body of revolution having a turbulent boundary layer. The addition of the tail surfaces having the trailing edges at or near the base of the body resulted in a large increase...
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| Format: | Government Document Book |
| Language: | English |
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Washington, D.C. :
National Advisory Committee for Aeronautics,
1951.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2360. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/2360
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| Y 3.N 21/5:6/2360 | Available Place a Hold |