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Development of a boundary-layer-type solver based on simultaneous iteration technique for axisymmetric separated flowsA boundary-layer-type solver is developed for the numerical solution of axisymmetric separated flows. A new fully implicit coupling scheme for the viscous and inviscid regions is demonstrated. This fully implicit coupling technique is similar to the work of Carter, Veldman, and an extension of an earlier work of Halim and Hafez. A comparison is made for the convergence rate using this new fully implicit coupling technique and the semiimplicit coupling of Halim and Hafez. Numerical results using the fully implicit coupling are obtained for laminar incompressible separated flows, including a boattail and a series of trough geometries. Also, the near-wake flow problem is considered using the present formulation. A clear conclusion of this investigation is that the present scheme using the fully implicit coupling method converges at a faster rate than the semiimplicit coupling and the partially parabolized Navier-Stokes (PPNS) procedures.
Document ID
19850058790
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Halim, A. A. M.
(Joint Institute for Advancement of Flight Sciences Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 85-1505
Report Number: AIAA PAPER 85-1505
Meeting Information
Meeting: Computational Fluid Dynamics Conference
Location: Cincinnati, OH
Start Date: July 15, 1985
End Date: July 17, 1985
Accession Number
85A40941
Funding Number(s)
CONTRACT_GRANT: NCC1-47
CONTRACT_GRANT: NAG1-573
Distribution Limits
Public
Copyright
Other

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