Supercritical Airfoil Technology in Compressor Cascades: Comparison of Theoretical and Experimental Results-Reference-Cited by-同舟云学术

Supercritical Airfoil Technology in Compressor Cascades: Comparison of Theoretical and Experimental Results

Published:1979-06 Issue:6 Volume:17 Page:594-600
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Stephens H. E.¹

Affiliation:

1. Pratt & Whitney Aircraft Group, East Hartford, Conn.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.61182

Reference15 articles.

1. Design of Supercritical Aerofoils

2. A Theory of Supercritical Wing Sections, with Computer Programs and Examples

3. Supercritical Wing Sections II

4. Kacprzynski, J. J., Ohman, L. H., Garabedian, P. R., and Korn, D. G. "Analysis of the Flow Past a Shockless Lifting Airfoil in Design and Off-Design Conditions," Aeronautical Report LR-554, National Research Council of Canada, Ottawa, 1971.

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