3 edition of Navier-Stokes simulation of wind-tunnel flow using LU-ADI factorization algorithm found in the catalog.
Navier-Stokes simulation of wind-tunnel flow using LU-ADI factorization algorithm
by National Aeronautics and Space Administration, Ames Research Center in Moffett Field, Calif
Written in English
|Statement||Shigeru Obayashi, Kozo Fujii and Sharad Gavali.|
|Series||NASA technical memorandum -- 100042.|
|Contributions||Fujii, Kozo., Gavali, Sharad., Ames Research Center.|
|The Physical Object|
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Get this from a library. Navier-Stokes simulation of wind-tunnel flow using LU-ADI factorization algorithm. [Shigeru Obayashi; Kozo Fujii; Sharad Gavali; Ames Research Center.]. Viscous Compressible Flow Simulations Using Supercomputers. Authors; K., “Improvements in Efficiency aand Reliability for Navier-Stokes Computations using the LU-ADI Factorization Algorithm,” to appear as AIAA PaperReno, Nevada, January, S., “Navier-Stokes Simulation of Transonic Flows over Wing-Fuselage Author: Kozo Fujii.
Computational methods are now pervasive in the science of aerodynamics. Because previously existing numerical methods proved inadequate for fluid flow simulations, the emergence of computational fluid dynamics (CFD) as a distinct discipline has sparked the development of an entirely new class of algorithms and a supporting body of theory, which are the main theme of this article.
Unsteady flow over an airfoil inside a wind tunnel with and without transpiration. TEDESCHI and; Numerical simulation of unsteady flow in an axisymmetric shear layer.
SCOTT and; Improvements in efficiency and reliability for Navier-Stokes computations using the LU-ADI factorization algorithm. OBAYASHI, K. KUWAHARA. The LU-ADI factorization algorithm for the Navier-Stokes computations has been developed by using the diagonally dominant LU factorization.
The space variable time stepping technique is also. Adaptation of Turbulence Models to a Navier-Stokes Solver Article (PDF Available) in Modelling, Measurement and Control B 76(6) January with Reads How we measure 'reads'. () Numerical Simulation of One-Dimensional Two-Phase Flow Using a Pressure-Based Algorithm.
Numerical Heat Transfer, Part A: Applications() High-order interpolation schemes for shear instability by: SOLUTIONS OF THE EULER EQUATIONS FOR TRANSONIC AND SUPERSONIC AIRCRAFT G. V O L P E Grumman Corporate Research Center, Bethpage, NYU.S.A.
Abstract--A method for numerically computing steady incompressible flow fields about fighter-type aircraft at transonic and supersonic speeds is : G.
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