Effect of ratio of wall boundary-layer thickness to jet diameter on mixing of a normal hydrogen jet in a supersonic stream /
by Charles R. McClinton.

Description

Main Author

McClinton, Charles R.

Related Names

Langley Research Center.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration ; 1974.

Subjects

Aerodynamics, Supersonic.
Boundary layer.
Jets > Jets / Fluid dynamics.
Fuel pumps.
Airplanes > Airplanes / Ramjet engines.

Note

Prepared at Langley Research Center.
Cover title.

Physical Description

42 p. : ill. ; 27 cm.

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