Accession Number:

AD0271821

Title:

METHOD OF INVESTIGATING BOUNDARY LAYER IN A NEW TYPE WORKING SECTION

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1962-02-09

Pagination or Media Count:

1.0

Abstract:

A turbulent boundary layer in the presence of a longitudinal pressure gradient is studied. Obtained were distributions of velocities in free flow and in flows moving along a plate and along a pan. Author

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE