Accession Number : AD0271821

Title :   METHOD OF INVESTIGATING BOUNDARY LAYER IN A NEW TYPE WORKING SECTION

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : MKHITARYAN,A.M. ; MAKSIMOV,V.S.

Report Date : 09 FEB 1962

Pagination or Media Count : 1

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)

Descriptors :   *LAMINAR BOUNDARY LAYER, *TURBULENCE, *WIND TUNNELS, GASES

Distribution Statement : APPROVED FOR PUBLIC RELEASE