Altitude-performance and Reynolds number investigation of centrifugal-flow-compressor turbojet engine

Wilsted, H. D., Grey, R. E.
naca-rm-e51b07
1951


The performance of a centrifugal-flow-compressor turbojet engine was investigated over a range of simulated-flight conditions from sea level to 65,000 feet at flight Mach numbers of 0.27 to 1.25.

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