Accession Number : ADA317068
Title : Theoretical Investigation of 3-D Shock Wave Turbulent Boundary Layer Interactions.
Descriptive Note : Final rept. 1 Oct 92-31 Jul 96,
Corporate Author : RUTGERS - THE STATE UNIV PISCATAWAY NJ DEPT OF MECHANICAL AND AEROSPACE ENGIN EERING
Personal Author(s) : Knight, Doyle D.
PDF Url : ADA317068
Report Date : 18 SEP 1996
Pagination or Media Count : 46
Abstract : This report summarizes the research project Theoretical Investigation of 3-D Shock Wave - Turbulent Boundary Layer Interactions during the period 1 October 1992 to 31 July 1996. The principal objectives of the research are the investigation of 3-D shock wave-turbulent boundary layer interactions (3-D turbulent interactions) for complex configurations (e.g., asymmetric shock), and the investigation of the accuracy of Chien's k - epsilon turbulence model, a newly developed Reynolds Stress Equation turbulence model and a k - epsilon model with a new low Reynolds number correction for 3-D turbulent interactions, with specific focus on the ability to predict surface heat transfer and skin friction. Accomplishments during the project include the development of a Reynolds Stress Equation (RSE) model (including determination of all constants), and computation of 3-D asymmetric and symmetric shock interactions at Mach 4 using Chien's k - epsilon turbulence model, the RSE model and the k - epsilon model with the new low Reynolds number correction. The report also provides a list of publications, scientific interactions and personnel.
Descriptors : *SHOCK WAVES, *TURBULENT BOUNDARY LAYER, *COMPUTATIONAL FLUID DYNAMICS, HEAT TRANSFER, MATHEMATICAL MODELS, STRESS ANALYSIS, TURBULENCE, FLOW FIELDS, MACH NUMBER, NAVIER STOKES EQUATIONS, FLOW SEPARATION, PRESSURE DISTRIBUTION, REYNOLDS NUMBER, THERMAL STRESSES, SKIN FRICTION, BOUNDARY LAYER FLOW, MOMENTUM TRANSFER, THREE DIMENSIONAL FLOW.
Subject Categories : Fluid Mechanics
Distribution Statement : APPROVED FOR PUBLIC RELEASE