Operational method of determining initial contour of and pressure field about a supersonic jet /
by Gerald W. Englert.

Description

Main Author: Englert, Gerald W.
Related Names: Lewis Research Center.
Language(s): English
Published: Washington, [D.C.] : National Aeronautics and Space Administration, 1960.
Subjects: Problem solving.
Laplace transformation.
Flat plates.
Boundary layers.
Supersonic flow.
Pressure distribution.
Jet exhaust.
Flow equations.
Exhaust nozzles.
Contours estimates.
Note: "NASA TN D-279."
"Lewis Research Center, Cleveland, Ohio."
"April 1960."
Cover title.
Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 10/11/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890068025_1989068025.pdf.
Physical Description: 37 p. : ill. ; 26 cm.
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