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International Journal of Rotating Machinery
Volume 5, Issue 2, Pages 89-98
http://dx.doi.org/10.1155/S1023621X99000081

Turbulence Amplification with Incidence at the Leading Edge of a Compressor Cascade

1Code AA/Hg, Department of Aeronautics and Astronautics, Naval Postgraduate School, 699 Dyer Rd, Rm 137, Monterey, CA 93943-5106, USA
2Flow Application Research Fremont, California, USA

Received 28 October 1997; Revised 19 March 1998

Copyright © 1999 Hindawi Publishing Corporation. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

How to Cite this Article

Garth V. Hobson, Bryce E. Wakefield, and William B. Roberts, “Turbulence Amplification with Incidence at the Leading Edge of a Compressor Cascade,” International Journal of Rotating Machinery, vol. 5, no. 2, pp. 89-98, 1999. https://doi.org/10.1155/S1023621X99000081.