Turbulent Shear-Layer/Shock-Wave Interaction.
Abstract
This report reviews presentations given at the September 1985 symposium of the International Union of Theoretical and Applied Mechanics and concludes that calculation of two-dimensional shock-wave/boundary-layer interaction problems is advancing well. For three-dimensional flows, accurate numerical calculation needs more experimental data to clarify the mechanisms and flow structures involved. Of greatest priority in this area is obtaining accurate unsteady measurements so that the mechanisms of shock oscillation and its results on the flow field can be better understood. Keywords: Boundary layer, Fluid mechanics, Fluid dynamic properties, and Boundary value problems.
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 01, 1986
- Accession Number
- ADA166934
Entities
People
- Eugene F. Brown
Organizations
- Office of Naval Research