Accession Number:

AD0271821

Title:

METHOD OF INVESTIGATING BOUNDARY LAYER IN A NEW TYPE WORKING SECTION

Personal Author(s):

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Report Date:

1962-02-09

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

Pages:

0001

Descriptors:

File Size:

0.00MB

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