Accession Number:

AD0420660

Title:

WIND TUNNEL,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1963-07-16

Pagination or Media Count:

4.0

Abstract:

A wind tunnel has been designed for the purpose of investigating boundary layer in a semirestricted stream under conditions of gradientless and gradient flow at greater flow velocities and constant pressure over a length of ten calibers of pressure nozzle. The working section is made in form of a rectangular trough with solid bottom and side walls and free flexible upper wall. Author

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE