Accession Number:

ADP007949

Title:

Some Aspects of Shock Wave Boundary Layer Interaction Relevant to Intake Flows,

Descriptive Note:

Corporate Author:

CRANFIELD INST OF TECH (UNITED KINGDOM)

Personal Author(s):

• Stollery, J. L.

Report Date:

1990-12-01

Pagination or Media Count:

14.0

Abstract:

This paper discusses four main topics 1 Two dimensional shock induced separation, 2 Three dimensional glancing interaction, 3 Shockshock 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