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NASA NTRS · 19650013746

Compressor design requirements

Bullock, R. O.·Prasse, E. I.

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Abstract

Cycle analysis of turbojet and turboprop engines - axial flow compressor requirements for gas turbine engines

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AXIAL FLOW COMPRESSOR TURBOPROP ENGINE TURBOJET ENGINE GAS TURBINE

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Bullock, R. O., Prasse, E. I.. 1965-01-01. Compressor design requirements. https://ntrs.nasa.gov/citations/19650013746

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