Theoretical augmentation of turbine-propeller engine by compressor-inlet water injection, tail-pipe burning, and their combination / Reece V. Hensley.
A theoretical evaluation of performance of turbine propeller engines with augmentation by water injection, tail-pipe burning, and their combination was made. The investigation cover the flight conditions for which each method of augmentation was most suitable for Mach numbers up to 1.1 and altitudes...
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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) ;
2672. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/2672
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| Y 3.N 21/5:6/2672 | Available Place a Hold |