Published April 1968
| Accepted Version
Journal Article
Open
Quasi Two-Dimensional Flows Through a Cascade
- Creators
- Mani, R.
- Acosta, A. J.
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.
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.Attached Files
Accepted Version - Quasi_Two-Dimensional_flows.Paper_No.67-WA-FE-9.pdf
Files
Quasi_Two-Dimensional_flows.Paper_No.67-WA-FE-9.pdf
Files
(2.0 MB)
| Name | Size | Download all |
|---|---|---|
|
md5:f6e6e847e8e0d6b679b30d819cdb47bb
|
2.0 MB | Preview Download |
Additional details
- Eprint ID
- 49079
- Resolver ID
- CaltechAUTHORS:20140829-144332902
- Nonr 220(59)
- Office of Naval Research (ONR)
- Created
-
2014-08-29Created from EPrint's datestamp field
- Updated
-
2021-11-10Created from EPrint's last_modified field