A theoretical estimate of the effects of compressibility on the performance of a helicopter rotor in various flight conditions / Alfred Gessow and Almer D. Crim.
The effects of compressibility arising from high-tip-speed operation on the flapping, thrust, and power of a helicopter rotor over a wide range of forward fkight conditions are investigated by the use of numerical methods.
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1956.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3798. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3798
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| Y 3.N 21/5:6/3798 | Available Place a Hold |