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contributor authorUbaldo Cella
contributor authorArthur Rizzi
date accessioned2017-05-08T21:16:01Z
date available2017-05-08T21:16:01Z
date copyrightApril 2000
date issued2000
identifier other%28asce%290893-1321%282000%2913%3A2%2847%29.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44917
description abstractNavier-Stokes Multiblock code solves the fully coupled system of equations simultaneously using a cell-centered finite-volume approach. This note assesses the sensitivity to some turbulence models and numerical schemes implemented in Navier-Stokes Multiblock when computing two test cases in standard mode, i.e., without tuning the code to these two cases. The cases are (1) subsonic flow around the MS(1)-0313 airfoil, and (2) transonic flow around the ONERA M6 wing, using various combinations of models (algebraic Baldwin-Lomax or Granville, one-equation Spalart-Allmaras, or the two-equation
publisherAmerican Society of Civil Engineers
titleSensitivity to Physical and Numerical Modeling in Navier-Stokes Simulations
typeJournal Paper
journal volume13
journal issue2
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)0893-1321(2000)13:2(47)
treeJournal of Aerospace Engineering:;2000:;Volume ( 013 ):;issue: 002
contenttypeFulltext


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