Reduction of acoustic disturbances in the test section of supersonic wind tunnels by laminarizing their nozzle and test section wall boundary layers by means of suction /
by W. Pfenninger and J. Syberg.

Description

Main Author

Pfenninger, W.

Related Names

Syberg, J.
Langley Research Center.
Boeing Commercial Airplane Company.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration ; 1974.

Subjects

Laminar flow.
Boundary layer.
Jet nozzles > Jet nozzles / Noise.
Supersonic wind tunnels.

Note

"Prepared by Boeing Commercial Airplane Company ... for Langley Research Center."
Cover title.

Physical Description

iii, 303 p. : ill. ; 27 cm.

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