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Type: BOOK - Published: 1948 - Publisher:
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Type: BOOK - Published: 1951 - Publisher:
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-inl
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Pages: 608
Pages: 608
Type: BOOK - Published: 1950 - Publisher:
Charts are presented by means of which the jet pressure ratio that give optimum division of power between propeller and jet for maximum total thrust power may b
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Type: BOOK - Published: 1957 - Publisher:
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Pages: 542
Pages: 542
Type: BOOK - Published: 1950 - Publisher: