NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Partially-Averaged Navier Stokes Model for Turbulence: Implementation and ValidationPartially-averaged Navier Stokes (PANS) is a suite of turbulence closure models of various modeled-to-resolved scale ratios ranging from Reynolds-averaged Navier Stokes (RANS) to Navier-Stokes (direct numerical simulations). The objective of PANS, like hybrid models, is to resolve large scale structures at reasonable computational expense. The modeled-to-resolved scale ratio or the level of physical resolution in PANS is quantified by two parameters: the unresolved-to-total ratios of kinetic energy (f(sub k)) and dissipation (f(sub epsilon)). The unresolved-scale stress is modeled with the Boussinesq approximation and modeled transport equations are solved for the unresolved kinetic energy and dissipation. In this paper, we first present a brief discussion of the PANS philosophy followed by a description of the implementation procedure and finally perform preliminary evaluation in benchmark problems.
Document ID
20050182919
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Girimaji, Sharath S.
(Texas A&M Univ. College Station, TX, United States)
Abdol-Hamid, Khaled S.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
May 12, 2005
Subject Category
Instrumentation And Photography
Report/Patent Number
AIAA Paper 2005-0502
Report Number: AIAA Paper 2005-0502
Meeting Information
Meeting: 43rd AIAA Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 10, 2005
End Date: January 13, 2005
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
OTHER: 23-781-10-12
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available