The aerodynamic design of supersonic propellers from structural considerations / Jerome B. Hammack.
A solution for radial distribution of cross-sectional area of supersonic propellers so that blade sections operate at maximum allowable centrifugal stress is given. The aerodynamic characteristics of some propellers designed by this method for Mach numbers from 0.9 to 2.4 for advance ratios of 2.0 a...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1952.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2851. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/2851
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| Y 3.N 21/5:6/2851 | Available Place a Hold |