Effect of heat and power extraction on turbojet-engine performance.
4 - Analytical determination of effects of hot-gas bleed /
Stanley L. Koutz.
Description
- Language(s)
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English
- Published
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Washington, D.C. : National Advisory Committee for Aeronautics, 1951.
- Summary
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In general, with a turbojet engine operating at constant engine speed, bleeding gas from the tail pipe at constant tail-pipe-nozzle area and reduced turbine-inlet temperature caused 2.5 to 4 times as great a loss in thrust as bleeding gas at constant turbine-inlet temperature and reduced tail-pipe-nozzle area.
Generalized working charts are presented with which the performance of a turbojet engine operating with tail-pipe gas bleed can be determined. From these generalized working charts, the performance of an engine operating with tail-pipe gas bleed at several typical flight conditions and modes of engine operation is calculated. A method of determing the performance of a turbojet engine with turbine-inlet bleed from the performance with compressor-outlet bleed is also given.
- Note
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NACA TN No. 2304.
"March 1951."
- Physical Description
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43 p. :
ill. ;
28 cm.
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