Aeromechanics Technology. Volume 1. Task 1. Three-Dimensional Euler/Navier-Stokes Aerodynamic Method (TEAM) Enhancements

Abstract

McDonnell Douglas has implemented a Johnson-King turbulence model into the Wright Laboratory TEAM code. Solutions were obtained for several test cases using the standard Baldwin-Lomax model and the incorporated Johnson-King model. Comparisons with experimental data were made where possible. General agreement was seen between the two turbulence models; however, poor agreement with the experimental data was noted for the Onera M6 wing test case. Grid sensitivity studies and further calibration of the TEAM code are needed. Computational fluid dynamics, Turbulence model, Navier-stokes

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Document Details

Document Type
Technical Report
Publication Date
Jul 26, 1994
Accession Number
ADA285713

Entities

People

  • R. K. Agarwal
  • T. P. Gielda

Organizations

  • McDonnell Douglas

Tags

Communities of Interest

  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Agreements
  • Air Force
  • Boundary Layer
  • Calibration
  • Computational Fluid Dynamics
  • Data Sets
  • Differential Equations
  • Dynamics
  • Equations
  • Experimental Data
  • Fluid Dynamics
  • Partial Differential Equations
  • Pressure Distribution
  • Standards
  • Three Dimensional
  • Turbulence
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Computational Fluid Dynamics (CFD)