Heat transfer measurements at Mach 8 on an aerodynamically controllable winged re-entry configuration :
part of an investigation of hypersonic flow separation and control characteristics /
Lawrence Meckler.

Description

Main Author

Meckler, Lawrence.

Related Names

United States. Air Force.
Air Force Flight Dynamics Laboratory (U.S.).
Grumman Aircraft Engineering Corporation. Research Department.

Language(s)

English

Published

Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964.

Subjects

Mach number.
Heat > Heat / Transmission.
Airplanes > Airplanes / Wings, Triangular.
Aerodynamics, Hypersonic.

Note

This report presents the results conducted by the Research Department of Grumman Aircraft Engineering Corporation, Bethpage, New York."
"September 1964."

Physical Description

xxiv, 413 pages : illustrations, figures, tables ; 28 cm.

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