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Limits of single-stage compression in centrifugal superchargers for aircraft
- Author / Creator
- Available as
- Online
- Summary
-
The limits of the single-stage compression in superchargers at the present state of development are determined by five factors. 1) by the rotor material; 2) by the formation of the flow; 3) by the ...
The limits of the single-stage compression in superchargers at the present state of development are determined by five factors. 1) by the rotor material; 2) by the formation of the flow; 3) by the manufacture of double shrouded rotors; 4) by the bearing problem; 5) by the drive method.
Details
- Creator
- by K. Kollmann
- Format
- Books
- Language
- English
- Publication
-
- Washington, D.C. : National Advisory Commitee for Aeronautics, 1940
- Physical Details
-
- 1 online resource (12, [4] pages) : illustrations, photographs
- data file
- OCLC
- on1372193397
- Title from title screen (viewed March 8, 2023)
- Date of issue: September 1940.
- Report numbers NACA-TM-954.
- Translated from Luftwissen. Vol. 7, No. 3, pp. 54-61, March 1940, by the National Advisory Commitee for Aeronautics.
- Includes bibliographical references (page 12)
- Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.