NASA NTRS · 19870061297
Supersonic through-flow fan design
Abstract
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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Schmidt, James F., Moore, Royce D., Wood, Jerry R., Steinke, Ronald J.. 1986-06-01. Supersonic through-flow fan design. https://ntrs.nasa.gov/citations/19870061297
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