NASA NTRS · 19690054722
A method for predicting the performance of high reaction supersonic compressor blade sections.
Abstract
Supersonic compressor blade sections performance prediction near maximum pressure ratio and efficiency by analyzing flow processes
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Boxer, E.. 1969-06-01. A method for predicting the performance of high reaction supersonic compressor blade sections.. https://ntrs.nasa.gov/citations/19690054722
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