Effect of advance ratio on flight performance of a modified supersonic propeller / Jerome B. Hammack and Thomas C. O'Bryan.
Results are presented of a flight investigation to determine the aerodynamic characteristics of a supersonic propeller modified by the incorporation of higher than optimum advance angles. The propeller was designed for a forward Mach number of 0.95, an advance ratio of 3.2, and a power coefficient o...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington :
National Advisory Committee for Aeronautics,
[1958]
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
4389. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/4389
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| Y 3.N 21/5:6/4389 | Available Place a Hold |