Axisymmetric supersonic flow in rotating impellers /
Arthur W. Goldstein.
Description
- Language(s)
-
English
- Published
-
Washington, D.C. : National Advisory Committee for Aeronautics, 1951.
- Summary
-
General equations are developed for isentropic frictionless, axisymmetric compressible flow in rotating impellers with blade forces eliminated in favor of the blade-surface function. The characteristic equations for supersonic flow are developed and a computing technique is utilized to find the effect of variations of design parameters on internal flow and work-input distribution.
- Note
-
NACA TN No. 2388.
"June 1951."
- Physical Description
-
36 p. :
ill. ;
28 cm.
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