Approximate method for determining equilibrium operation of compressor component of turbojet engine / Merle C. Huppert.
A method is presented for estimating the equilibrium operating line for a compressor as a component part of a turbojet engine. The performance characteristics of the combustor, turbine, and jet nozzle are treated in a simplified manner, so that the suitability of a given compressor for jet-engine ap...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1955.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3517. |
| Subjects: |
PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3517
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| Y 3.N 21/5:6/3517 | Available Place a Hold |