Accession Number:

ADA055952

Title:

M=3 Turbulent Boundary Layer Measurements at very High Reynolds Numbers.

Descriptive Note:

Interim rept. Jan 76-Jul 77 on Phase 1,

Corporate Author:

AIR FORCE FLIGHT DYNAMICS LAB WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1977-10-01

Pagination or Media Count:

230.0

Abstract:

Experimental turbulent boundary layer measurements were made. Data was generated at supersonic speeds and very high Reynolds numbers to determine the effect of both unit and length Reynolds numbers on boundary layer profiles, thickness parameters, and skin friction measurements.

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE