Unsteady turbulent boundary layers in two-dimensional, incompressible flow.The paper presents the results of some calculations aimed at studying the characteristics of turbulent boundary layers in unsteady flow. The calculations were performed using the method of Singleton and Nash, which is based on the turbulent kinetic energy equation. Emphasis is placed on the approach to zero wall stress, and the results show the extent to which onset of this condition can be delayed by the effects of time dependence. The delay is not associated merely with alleviation of the pressure gradients, and quasi-steady methods cannot readily be used to calculate this type of flow.
Document ID
19730051403
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Nash, J. F. (Scientific and Business Consultants, Inc. Smyrna, Ga., United States)
Carr, L. W. (U. S. Army, Air Mobility Research and Development Laboratory, Moffett Field Calif., United States)
Singleton, R. E. (Lockheed-Georgia Co. Marietta, Ga., United States)
Date Acquired
August 7, 2013
Publication Date
July 1, 1973
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 73-650Report Number: AIAA PAPER 73-650
Meeting Information
Meeting: Fluid and Plasma Dynamics Conference
Location: Palm Springs, CA
Start Date: July 16, 1973
End Date: July 18, 1973
Sponsors: American Institute of Aeronautics and Astronautics