Affiliation:
1. University of Wisconsin-Milwaukee
Publisher
American Institute of Aeronautics and Astronautics
Reference16 articles.
1. 1Bliss, D.B., 1976, Method of and Apparatus for Preventing Leading Edge Shockand Shock Related Noise in Transonic and Supersonic Blades andLike, US Patent 3989406.
2. An Implicit Scheme for Cascade Flow and Heat Transfer Analysis
3. Computational analysis of pitch-width effects on the secondary flows of turbine blades
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