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Application of the k-epsilon-v(exp 2) model to multi-component airfoilsFlow computations around two-element and three-element configurations are presented and compared to detailed experimental measurements. The k-epsilon-v(exp 2)(bar) model has been applied and the ability of the model to capture streamline curvature effects, wake-boundary layer confluence, and laminar/turbulent transition is discussed. The numerical results are compared to experimental datasets that include mean quantities (velocity and pressure coefficient) and turbulent quantities (Reynolds normal and shear stresses).
Document ID
19970014653
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Iaccarino, G. (Italian Aerospace Research Center Naples, Italy)
Durbin, P. A. (Stanford Univ. Stanford, CA United States)
Date Acquired
August 17, 2013
Publication Date
December 1, 1996
Publication Information
Publication: Studying Turbulence Using Numerical Simulation Databases
Volume: Part 6
Subject Category
Aerodynamics
Accession Number
97N17994
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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