Accession Number:

AD0677093

Title:

EXPERIMENTAL STUDY OF A SONIC TURBULENT BOUNDARY LAYER ON A PLATE WITH A BLAST,

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CALIF

Personal Author(s):

Report Date:

1960-10-01

Pagination or Media Count:

14.0

Abstract:

Experiments on the study of the effect of a uniform air blast on the profile of the velocity in a boundary layer were carried out on an instrument composed of a sonic aerodynamic tube with open working part in which the porous model is located. The instrument guaranteed a blast of air of a velocity up to 75 m.sec., and a temperature up to 600C at the discharge from the nozzle. Author

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE