Static aerodynamic characteristics of a model of a typical subsonic jet-transport airplane at Mach numbers from 0.40 to 1.20 /
by Eugene N. Brooks, Jr., John P. Decker, and James A. Blackwell, Jr.

Description

Main Author: Brooks, Eugene N.
Related Names: Blackwell, James A.
Decker, John P.
Langley Research Center.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration ; 1967.
Subjects: Transport aircraft.
Subsonic flow.
Subsonic aircraft.
Static aerodynamic characteristics.
Mach number.
Jet aircraft.
Gas jets.
Angle of attack.
Note: "NASA TM X-1345."
"Langley Research Center, Langley Station, Hampton, Va."
"February 1967"--Cover.
Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 8/02/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19670009071_1967009071.pdf.
Physical Description: 37 p. : ill. ; 27 cm.
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