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Quasi Two-Dimensional Flows Through a Cascade

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. 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
Related URLs:
URLURL TypeDescription
http://gasturbinespower.asmedigitalcollection.asme.org/article.aspx?articleid=1417530PublisherArticle
http://dx.doi.org/10.1115/1.3609146DOIArticle
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.
Funders:
Funding AgencyGrant Number
Office of Naval Research (ONR)Nonr 220(59)
Subject Keywords:Flow (Dynamics) , Cascades (Fluid dynamics) , Airfoils , Axial flow , Channels (Hydraulic engineering)
Issue or Number:2
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: Kristin Buxton
Deposited On:29 Aug 2014 21:48
Last Modified:03 Oct 2019 07:10

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