NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Advisory – Planned Maintenance: On Monday, July 15 at 9 PM Eastern the STI Compliance and Distribution Services will be performing planned maintenance on the STI Repository (NTRS) for approximately one hour. During this time users will not be able to access the STI Repository (NTRS).

Back to Results
Numerical Simulation of Flow in a Whirling Annular Seal and Comparison With ExperimentsThe turbulent flow field inside a whirling annular seal was simulated by using SCISEAL, a three-dimensional computational fluid dynamics code. The rotor center described a circular synchronous whirl. A rotating frame transformation was used to make the problem quasi-steady. The flow field at an axial Reynolds number of 24,000 and a Taylor number of 6600 was simulated. The standard kappa-epsilon model with wall functions and the low-Reynolds-number model were used to treat turbulence. An experimentally measured velocity field was used at the inlet boundary. Numerical predictions of the velocities and the stator wall pressures compared well with experimental data. Both turbulence models yielded nearly the same results. The capability of the SCISEAL code to analyze this complex flow field was demonstrated; the isotropic turbulence models performed adequately on this nonisotropic turbulence flow.
Document ID
20030063012
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Athavale, M. M.
(CFD Research Corp. Huntsville, AL, United States)
Hendricks, R. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Steinetz, B. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
March 1, 1996
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.15:107117
E-10026
NASA-TM-107117
Meeting Information
Meeting: Sixth International Symposium on Transport Phenomena and Dynamics of Rotating Machinery
Location: Honolulu, HI
Country: United States
Start Date: February 25, 1996
End Date: February 29, 1996
Sponsors: Pacific Centre of Thermal Fluids Engineering, United States Turbo and Power Machinery Research Center
Funding Number(s)
WORK_UNIT: WU 242-20-06
CONTRACT_GRANT: NAS3-25644
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available