Catalog Record: Effects of wing height on the stability and control characteristics at a mach number of 2.01 of a canard airplane configuration with a 70° delta wing | Hathi Trust Digital Library

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Effects of wing height on the stability and control characteristics at a mach number of 2.01 of a canard airplane configuration with a 70° delta wing / by Cornelius Driver.

Main Author: Driver, Cornelius.
Language(s): English
Published: Washington, [D.C.] : National Aeronautics and Space Administration, 1960.
Subjects: Airplanes > Wings, Triangular > Testing.
Mach number.
Stability of airplanes.
Note: Cover title.
"September 1960."
Physical Description: 30 p. : ill. ; 26 cm.
Original Format: Book
Locate a Print Version: Find in a library
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