Experimental, water droplet impingement data on two-dimensional airfoils, axisymmetric inlet and Boeing 737-300 engine inlet
Author:
Affiliation:
1. Wichita State University, KS
2. Boeing Military Airplane Co., Wichita, KS
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1987-97
Reference31 articles.
1. HlGH ,IG*T MARK
2. Figigwe 15. Pilot 06 Auehage Output Data un. Swdace mcasured from the comprcssor face (X.0) for the 737-300 inict and from the highlight for the axisymmetric
3. for the Boeing 737-300 inlet at angles of attack 0 and
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