NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
A turbulence model for nonequilibrium adverse pressure gradient flowsThis paper presents a method for calculating compressible adverse pressure gradient boundary layers by using an algebraic eddy viscosity turbulence model that has been modified for variable pressure gradient and turbulence memory effects. The pressure gradient corrections are based on previous incompressible data correlations. Several methods for including the effects of turbulence memory are evaluated. A new lag model, which gives good agreement with available experimental data, is developed. Finally, a correlation is developed for the lag length parameter employed in the model as a function of the known experimental flow variables.
Document ID
19760054083
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Horstman, C. C.
(NASA Ames Research Center Experimental Fluid Dynamics Branch, Moffett Field, Calif., United States)
Date Acquired
August 8, 2013
Publication Date
July 1, 1976
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 76-412
Meeting Information
Meeting: Fluid and Plasma Dynamics Conference
Location: San Diego, CA
Start Date: July 14, 1976
End Date: July 16, 1976
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
76A37049
Distribution Limits
Public
Copyright
Other

Available Downloads

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