Experimental investigation of an axial-flow compressor inlet stage operating at transonic relative inlet mach numbers, III - Blade-row performance of stage with transonic rotor and subsonic stator at corrected tip speeds of 800 and 1000 feet per second,
by Francis C. Schwenk, Seymour Lieblein and George W. Lewis, Jr., National Advisory Committee for Aeronautics, Washington, D.C. (Research memorandum E53G17), September1953
File — Box: 3, Folder: 16.1
Collection Scope and Contents
From the Collection:
The collection consists of reports and papers on the subjects of pumps, turbines, fans, metering and flow (hydraulics).
Dates
- Creation: September1953
Creator
- From the Collection: Iversen, Harold W. (Person)
Languages
From the Collection:
The collection is in English.
Access
The collection is open for research.
Extent
From the Collection: 14.0 Linear Feet (14 boxes)
Repository Details
Part of the Water Resources Collections & Archives Repository
Contact:
University of California
Rivera Library
P.O. Box 5900
Riverside CA 92517-5900 United States
specialcollections@ucr.edu
University of California
Rivera Library
P.O. Box 5900
Riverside CA 92517-5900 United States
specialcollections@ucr.edu