Influence of wall boundary layer upon the performance of an axial-flow fan rotor /
by Emanuel Boxer.

Description

Main Author

Boxer, Emanuel.

Related Names

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

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, 1947./

Subjects

Boundary layer.
Axial flow compressors > Axial flow compressors / Blades > Axial flow compressors / Blades / Aerodynamics.

Note

"May 19, 1947"--Cover.
Caption title.

Physical Description

8, [13] p. : ill. ; 26 cm.

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