Effects of jet billowing on stability of missile-type bodies at Mach 3.85 /
by Reino J. Salmi.

Description

Main Author: Salmi, Reino J.
Related Names: Lewis Research Center.
Language(s): English
Published: Washington, [D.C.] : National Aeronautics and Space Administration, 1960.
Subjects: Zero angle of attack.
Static stability.
Static pressure.
Sonic nozzles.
Pressure ratio.
Pressure dependence.
Pitching moments.
Boundary layer separation.
Wind tunnel tests.
Missile bodies.
Mach number.
Jet flow.
Jet exhaust.
Flow distribution.
Aerodynamic interference.
Note: "NASA TN D-284."
"Lewis Research Center, Cleveland, Ohio."
"June 1960."
Cover title.
Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 10/12/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890068037_1989068037.pdf.
Physical Description: 17 p. : ill. ; 26 cm.
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