NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Behavior of a turbulent boundary layer subjected to sudden transverse strainData from two experiments on the development of the components of the Reynolds stress tensor after a sudden application of transverse strain are compared. Computations were based on four different turbulence models: a first-order mixing length model, a second-order two-equation eddy viscosity model, and two second-order Reynolds stress models. The second-order models do not produce dramatic improvements over the simple mixing length model. The Reynolds stress models still need development to represent the physics of shear-strained turbulence well. Finally, it is demonstrated that the assumption of a scalar eddy viscosity, often used in engineering calculations of three-dimensional boundary layers, is quite reasonable.
Document ID
19780038686
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Higuchi, H.
(Dynamics Technology, Inc. Torrance, Calif., United States)
Rubesin, M. W.
(NASA Ames Research Center Moffett Field, Calif., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 78-201
Report Number: AIAA PAPER 78-201
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Huntsville, AL
Start Date: January 16, 1978
End Date: January 18, 1978
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
78A22595
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available