Accession Number:

ADA014769

Title:

Research on Supersonic Turbulent Separated and Reattached Flows.

Descriptive Note:

Final rept. Jul 73-Apr 75,

Corporate Author:

PRINCETON UNIV N J GAS DYNAMICS LAB

Report Date:

1975-06-01

Pagination or Media Count:

89.0

Abstract:

Basic research programs are reported with fundamental applications to supersonic flight. The experimental studies made use of the unique capabilities of the high Reynolds number Mach 3 facility. The experimental programs concentrated on phenomena associated with incipient separation and separation of turbulent boundary layers over a large Reynolds number range. The reattachment phenomena of a shear layer was also studied in great depth.

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE