Accession Number : ADP007949
Title : Some Aspects of Shock Wave Boundary Layer Interaction Relevant to Intake Flows,
Corporate Author : CRANFIELD INST OF TECH (UNITED KINGDOM)
Personal Author(s) : Stollery, J. L.
Report Date : DEC 1990
Pagination or Media Count : 14
Abstract : This paper discusses four main topics: (1) 'Two dimensional' shock induced separation, (2) Three dimensional glancing interaction, (3) Shock/shock boundary layer interaction, and (4) Hypersonic viscous interaction. Wherever possible both laminar and turbulent flows are considered and reference is made to experimental data and to the results of mathematical modelling. The paper ends with some thoughts on future research topics and the facilities needed to pursue them.
Descriptors : *INTERACTIONS, *BOUNDARY LAYER FLOW, *SHOCK WAVES, BOUNDARIES, BOUNDARY LAYER, EXPERIMENTAL DATA, FACILITIES, LAYERS, PAPER, SEPARATION, SHOCK, THREE DIMENSIONAL, TURBULENT FLOW, AIR INTAKES, MATHEMATICAL MODELS.
Subject Categories : Fluid Mechanics
Distribution Statement : APPROVED FOR PUBLIC RELEASE