An analysis of the pressure distribution measured on a body of revolution at transonic speeds in the slotted test section of the Langley 8-foot transonic tunnel /
By Bruce B. Estabrooks.

Description

Main Author

Estabrooks, Bruce B.

Related Names

Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics.

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, 1952.

Subjects

Aerodynamics, Transonic.
Body of revolution.
Aerodynamic load.

Note

"June 25, 1952."

Physical Description

42 p. : ill. ; 27 cm.

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