Loads induced on a flat-plate wing by an air jet exhausting perpendicularly through the wing and normal to a free-stream flow of mach number 2.0 /
by Joseph J. Janos

Description

Main Author

Janos, Joseph J.

Related Names

United States. National Aeronautics and Space Administration.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration : [1961]

Subjects

Stability and control.
Space vehicles.
Fluid mechanics.
Atmospheric entry.
Aerodynamics, missiles and space vehicles.
Aerodynamics, aircraft.

Note

Cover title.
"March 1961."
Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanics; Space vehicles; Stability and control.

Physical Description

21p.: ill. ; 26 cm.

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