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
Personal Author(s) : Bogdonoff,S. M. ; Vas,I. E. ; Settles,G. S. ; Simpers,G.
Report Date : JUN 1975
Pagination or Media Count : 89
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.
Descriptors : *Turbulent boundary layer, *Flow separation, *Supersonic characteristics, Research facilities, Reynolds number, Supersonic flight, Shear properties, Boundary layer flow, Static pressure, Flow visualization, Surface properties, Shock waves
Subject Categories : Fluid Mechanics
Distribution Statement : APPROVED FOR PUBLIC RELEASE