Accession Number:

ADA037441

Title:

Laminariscent Turbulent Boundary Layers: Experiments on Nozzle Flows.

Descriptive Note:

Technical rept.,

Corporate Author:

PURDUE UNIV LAFAYETTE IND PROJECT SQUID HEADQUARTERS

Personal Author(s):

Report Date:

1977-01-01

Pagination or Media Count:

107.0

Abstract:

Because a turbulent boundary layer in a nozzle undergoes strong acceleration, a laminariscent boundary layer with the benefit of a lower surface heat transfer rate can result for some short distance. Here several phenomena which accompany laminarescence produced by strong acceleration are examined for nozzle-flow and sink-flow accelerational distributions, respectively.

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE