Numerical Study of Turbulence Model Predictions for the MD 30P/30N and NHLP-2D Three-Element Highlift ConfigurationsThis report details calculations for the McDonnell-Douglas 30P/30N and the NHLP-2D three-element highlift configurations. Calculations were performed with the Reynolds averaged Navier-Stokes code ISAAC to study the effects of various numerical issues on high lift predictions. These issues include the effect of numerical accuracy on the advection terms of the turbulence equations, Navier-Stokes versus the thin-layer Navier-Stokes approximation, an alternative formulation of the production term, and the performance of several turbulence models. The effect of the transition location on the NHLP-2D flow solution was investigated. Two empirical transition models were used to estimate the transition location.
Document ID
19990024873
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Joseph H Morrison (Analytical Services & Materials (United States) Hampton, Virginia, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1998
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.26:208967NASA/CR-1998-208967Report Number: NAS 1.26:208967Report Number: NASA/CR-1998-208967