Measurements of a supersonic favorable-pressure-gradient turbulent boundary layer with heat Transfer :
part 1 -data compilation. /
Robert L. P. Voisinet and Roland E. Lee.

Description

Main Author

Voisinet, Robert L. P.

Related Names

Lee, Roland E., author.
Naval Ordnance Laboratory (White Oak, Md.)

Language(s)

English

Published

Silver Spring, Maryland : Naval Ordnance Laboratory, 1973.

Subjects

Fluid mechanics.
Wind tunnels.
Nozzles.
Heat > Heat / Transmission.
Skin friction (Aerodynamics)
Turbulent boundary layer.

Summary

The results of a detailed experimental investigation of the compressible turbulent boundary layer in a favorable-pressure-gradient flow are presented for zero, moderate and severe heat-transfer conditions. The studies were conducted on a flat nozzle wall at momentum thickness Reynolds numbers from 6,700 to 56,000 and at three wall-to-adiabatic-wall temperature ratios. An attempt was made to hold values of Clauser's pressure-gradient parameter constant. Complete profile measurements were taken with Pitot pressure probes and conical-equilibrium and fine-wire temperature probes. (Modified author abstract).

Note

12 December 1973.
AIRTASK A32 320/292/69/R009-02-030.

Physical Description

124 pages (various pagings) : illustrations ; 28 cm

Locate a Print Version

Find in a library

Viewability