Pressure measurements for Mach five flows over a blunt pyramidal configuration with aerodynamic controls :
part of an investigation of hypersonic flow separation and control characteristics /
Louis G. Kaufman II.

Description

Main Author

Kaufman, Louis G.

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

Airplanes > Airplanes / Dihedral wings.
Aerodynamics, Hypersonic.

Note

"January 1964."

Physical Description

vi, 243 pages : illustrations, figures, tables ; 28 cm.

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