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Computations of Three-Dimensional Steady and Unsteady Viscous Incompressible FlowsThe INS3D family of computational fluid dynamics computer codes is presented. These codes are used to as tools in developing and assessing algorithms for solving the incompressible Navier-Stokes equations for steady-state and unsteady flow problems. This work involves applying the codes to real-world problems involving complex three-dimensional geometries. The algorithms utilized include the method of pseudocompressibility including both central and upwind differencing, several types of artificial dissipation schemes, approximate factorization, and an implicit line-relaxation scheme. These codes have been validated using a wide range of problems including flow over a backward-facing step, driven cavity flow, flow through various types of ducts, and steady and unsteady flow over a circular cylinder. Many diverse flow applications have been solved using these codes including parts of the Space Shuttle Main Engine, problems in naval hydrodynamics, low-speed aerodynamics, and biomedical fluid flows. The presentation details several of these, including the flow through a Space Shuttle Main Engine inducer, vortex shedding behind a circular cylinder, and flow through an artificial heart.
Document ID
19910001539
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Dochan Kwak
(Ames Research Center Mountain View, United States)
Stuart E Rogers
(Ames Research Center Mountain View, United States)
Yoon, Seokkwan
(MCAT Institute Moffett Field, CA, United States)
Moshe Rosenfeld
(MCAT Institute Moffett Field, CA, United States)
Leon Chang
(MCAT Institute Moffett Field, CA, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1989
Publication Information
Publication: NASA Computational Fluid Dynamics Conference. Volume 1: Sessions 1-6
Publisher: National Aeronautics and Space Administration
Volume: 1
Subject Category
Aerodynamics
Report/Patent Number
NASA-CP-10038-VOL-1
Meeting Information
Meeting: NASA Computational Fluid Dynamics Conference
Location: Moffett Field, CA
Country: US
Start Date: March 7, 1989
End Date: March 9, 1989
Sponsors: National Aeronautics and Space Administration
Accession Number
91N10852
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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