Aerodynamic characteristics over a Mach number range of 1.40 to 2.78 of a rocket-propelled airplane configuration having a low 52.2° delta wing and an unswept horizontal tail. /
by Alan B. Kehlet.

Description

Main Author

Kehlet, Alan B.

Related Names

United States. National Adviosry Committee for Aeronautics.
Langley Aeronautical Laboratory.

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, 1958.

Subjects

Stability of airplanes.
Airplanes > Airplanes / Wings, Triangular.
Airplanes > Airplanes / Tail surfaces.
Airplanes > Airplanes / Rocket engines.
Aerodynamics, Supersonic.
Stability of airplanes.
Aerodynamics, Supersonic.
Airplanes > Airplanes / Rocket engines.
Airplanes > Airplanes / Tail surfaces.
Airplanes > Airplanes / Wings, Triangular.

Note

"March 6, 1958."

Physical Description

26 pages : illustrations ; 27 cm.

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