Axial Compressor Blade Optimization in the Low Reynolds Number Regime
Author:
Affiliation:
1. Nielsen Engineering & Research, Inc., Mountain View, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference21 articles.
1. Observations of Separated Laminar Flow on Axial Compressor Blading
2. The Experimental Cascade Performance of NACA Compressor Profiles at Low Reynolds Number
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