Mani, R. and Acosta, A. J. (1968) Quasi Two-Dimensional Flows Through a Cascade. Journal of Engineering for Gas Turbines and Power, 90 (2). pp. 119-127. ISSN 0742-4795. doi:10.1115/1.3609146. https://resolver.caltech.edu/CaltechAUTHORS:20140829-144332902
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Abstract
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.
| Item Type: | Article | |||||||||
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| 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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| Subject Keywords: | Flow (Dynamics) , Cascades (Fluid dynamics) , Airfoils , Axial flow , Channels (Hydraulic engineering) | |||||||||
| Issue or Number: | 2 | |||||||||
| DOI: | 10.1115/1.3609146 | |||||||||
| Record Number: | CaltechAUTHORS:20140829-144332902 | |||||||||
| Persistent URL: | https://resolver.caltech.edu/CaltechAUTHORS:20140829-144332902 | |||||||||
| Usage Policy: | No commercial reproduction, distribution, display or performance rights in this work are provided. | |||||||||
| ID Code: | 49079 | |||||||||
| Collection: | CaltechAUTHORS | |||||||||
| Deposited By: | INVALID USER | |||||||||
| Deposited On: | 29 Aug 2014 21:48 | |||||||||
| Last Modified: | 10 Nov 2021 18:39 |
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