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Published April 1968 | Accepted Version
Journal Article Open

Quasi Two-Dimensional Flows Through a Cascade


A thin airfoil theory is developed for airfoils spanning a slowly diverging or converging channel, the motivation being to predict, theoretically, the effect of varying axial velocity on the cascade performance of axial flow compressor rows.

Additional Information

Copyright © 1968 by ASME. Contributed by the Fluids Engineering Division for presentation at the Winter Annual Meeting, Pittsburgh, Pa., November 12-17, 1967, of the American Society of Mechanical Engineers. Manuscript received at ASME Headquarters, August 1, 1967. Paper No. 67--WA/FE-9. This research was accomplished with the support of the Office of naval research under Contract Nonr 220(59). The assistance of Mrs. Z. Harrison in the numerical calculations is gratefully acknowledged.

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Accepted Version - Quasi_Two-Dimensional_flows.Paper_No.67-WA-FE-9.pdf


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August 19, 2023
October 17, 2023