Supersonic through-flow fan design | Zendy

J. F. Schmidt | Zendy; R. D. Moore | Zendy; J. R. Wood | Zendy; R. J. Steinke | Zendy

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Supersonic through-flow fan design

Author(s) -

J. F. Schmidt,

R. D. Moore,

J. R. Wood,

R. J. Steinke

Publication year - 1987

Publication title -

23rd joint propulsion conference

Language(s) - English

Resource type - Conference proceedings

DOI - 10.2514/6.1987-1746

Subject(s) - computer science , choked flow , supersonic speed , flow (mathematics) , aerospace engineering , engineering , mechanics , physics

The NASA Lewis Research Center has embarked on a program to experimentally prove the concept of a supersonic through-flow fan which is to maintain supersonic velocities throughout the compression system with only weak shock-wave flow losses. The detailed design of a supersonic through-flow fan and estimated off-design performance with the use of advanced computational codes are described. A multistage compressor facility is being modified for the newly designed supersonic through-flow fan and the major aspects of this modification are briefly described.

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