Accession Number : ADA187642
Title : The Structure and Control of Three-Dimensional Shock Wave Turbulent Boundary Layer Interactions.
Descriptive Note : Annual rept. 15 Jul 86-14 Jul 87,
Corporate Author : PRINCETON UNIV N J GAS DYNAMICS LAB
Personal Author(s) : Bogdonoff, Seymour M
PDF Url : ADA187642
Report Date : 24 Nov 1987
Pagination or Media Count : 20
Abstract : A review of the work completed during the first year of research on the subject contract is presented. Papers and publications generated, staff, and students involved in research are noted, along with a brief description of the on-going program. Significant results have been obtained in defining the structure of the three-dimensional shock wave turbulent boundary layer interaction by combining detailed experiments with coordinated major computational programs. Keywords: Shock wave, Boundary layer, Supersonic.
Descriptors : *SHOCK WAVES, *TURBULENT BOUNDARY LAYER, *INTERACTIONS, *SUPERSONIC FLOW, COMPUTATIONS, THREE DIMENSIONAL FLOW, PRESSURE GRADIENTS, UNSTEADY FLOW, VORTICES, FLOW SEPARATION, PRESSURE, WALLS, FINS
Subject Categories : Fluid Mechanics
Distribution Statement : APPROVED FOR PUBLIC RELEASE