Turbulent heat-transfer prediction method for application to scramjet engines /
by S.Z. Pinckney.

Description

Main Author

Pinckney, S. Z. (Shimer Zane), 1934-

Related Names

Langley Research Center.

Language(s)

English

Published

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

Subjects

Combustion chambers > Combustion chambers / Cooling.
Turbulent boundary layer.
Heat > Heat / Transmission.
Airplanes > Airplanes / Ramjet engines > Airplanes / Ramjet engines / Cooling.

Note

Prepared at Langley Research Center.
Cover title.

Physical Description

64 p. : ill. ; 27 cm.

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