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Reynolds averaged Navier-Stokes computations of transonic flows The-state-of-the-artThe state of the art in computer simulations for transonic flowfields requiring solutions for the Navier-Stokes equations is assessed. It is noted that current simulations of transonic flowfields require comparisons with experimental results because the simulations are not free from discretization errors. Cases of turbulence are treated with weighted variables in a time-averaged scheme to yield Reynolds averaged Navier-Stokes equations. The turbulence is modeled in a first-order approach with a Reynolds stress tensor or a second-order approach where the tensor is obtained from the Navier-Stokes equations. The choice of coordinate systems and dependent variables for simulating the flow around airfoils is discussed, with particular attention to curvilinear coordinates. The determinations of boundary conditions is examined, along with numerical methods related to physical phenomena
Document ID
19820052024
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Mehta, U.
(NASA Ames Research Center Moffett Field, CA, United States)
Lomax, H.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1982
Subject Category
Aerodynamics
Meeting Information
Meeting: Transonic aerodynamics; Transonic Perspective Symposium
Location: Moffett Field, CA
Start Date: February 18, 1981
End Date: February 20, 1981
Accession Number
82A35559
Distribution Limits
Public
Copyright
Other

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