Second-Order-Accurate Calculation of Transonic Flow over Turbomachinery Cascades
Author:
Affiliation:
1. Pratt & Whitney Aircraft, East Hartford, Conn.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.61239
Reference14 articles.
1. Supercritical Airfoil Technology in Compressor Cascades: Comparison of Theoretical and Experimental Results
2. Supercritical Wing Sections II
3. Theory of viscous transonic flow over airfoils at high Reynolds number
4. On displacement thickness
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