Wing-on and wing-off longitudinal characteristics of an airplane configuration having a thin unswept wing of aspect ratio 3, as obtained from rocket-propelled models at Mach numbers from 0.8 to 1.4 /
by Clarence L. Gillis and A. James Vitale.

Description

Main Author: Gillis, Clarence L.
Related Names: Vitale, A. James.
Langley Research Center.
Language(s): English
Published: Washington, [D.C.] : National Aeronautics and Space Administration, 1959.
Subjects: Static stability.
Pitch (inclination).
Mach number.
Drag lift.
Aspect ratio.
Unswept wings.
Thin wings.
Rocket engines.
Aircraft models.
Aircraft configurations.
Note: "NASA TN D-7."
"Langley Research Center, Langley Field Va."
"March 1960."
Cover title.
Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 10/20/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890068082_1989068082.pdf.
Physical Description: 42 p. : ill. ; 26 cm.
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