Investigation of the effect of a guide-vane-rotor combination on inlet total-pressure distortions in a compressible fluid /
by George C. Ashby, Jr.

Description

Main Author: Ashby, George C.
Related Names: Langley Research Center.
Language(s): English
Published: Washington, [D.C.] : National Aeronautics and Space Administration, 1959.
Subjects: Subsonic speed.
Plates (structural members)
Jet aircraft.
Density (mass volume)
Compressors.
Rotors.
Pressure distribution.
Inlet pressure.
Inlet flow.
Guide vanes.
Flow distortion.
Compressible flow.
Note: "NASA TN D-123."
"Langley Research Center, Langley Field, Va."
"December 1959."
Title from cover.
Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 12/11/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890068383_1989068383.pdf.
Physical Description: 15 p. : ill. ; 26 cm.
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