Aerodynamic characteristics in pitch at a Mach number of 2.01 of several wing-body combinations with wedge-shaped bodies located above and below a 54.5 ̊swept delta wing /
Odell A. Morris.

Description

Main Author

Morris, Odell A.

Related Names

Langley Research Center.
United States. National Aeronautics and Space Administration.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration, 1963.

Subjects

Delta wing airplanes > Delta wing airplanes / Handling characteristics.
Pitching (Aerodynamics)
Interference (Aerodynamics)
Lift (Aerodynamics)
Mach number.
Space vehicles.

Physical Description

22 p. : ill. ; 27 cm.

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