Pressure measurements for mach five flows over winged re-entry configurations with aerodynamic controls.
Part II.
Conical cabin configuration /
Louis G. Kaufman.

Description

Main Author

Kaufman, Louis G.

Related Names

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

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

Heat > Heat / Transmission.
Airplanes > Airplanes / Wings, Swept-back.

Note

"February 1964."

Physical Description

vi, 203 pages : illustrations, figures, tables ; 28 cm.

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