Turbulence models and their application : efficient numerical methods with computer programs /Author: Cebeci, Tuncer
Publisher: New York : Springer, Berlin ; New York : Springer,
Date: c2004. This title can be found in 2 Iowa libraries.
Prediction of bypass transition with differential Reynolds stress models /Author: Westin, K. J. A.
Publisher: Delft, Netherlands : Delft University Press,
Date: 1998. This title can be found in 1 Iowa libraries.
Unsteady RANS method for surface ship boundary layer and wake and wave field /Author: Rhee, Shin-Hyung.
Publisher: [Place of publication not identified] : [publisher not identified],
Date: 1998. This title can be found in 1 Iowa libraries.
Supersonic flow calculation using a Reynolds-stress and an eddy thermal diffusivity turbulence modelFormat: [microform] /
Author: Sommer, T. P.
Publisher: [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;
Date: 1993. This title can be found in 2 Iowa libraries.
Application of a new K-[tau] model to near wall turbulent flowsFormat: [microform] /
Author: Thangam, S.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center,
Date: [1991] This title can be found in 1 Iowa libraries.
Development of a defect stream function, law of the wall/wake method for compressible turbulent boundary layersFormat: [microform] /
Author: Wahls, Richard A.
Publisher: Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;
Date: 1990. This title can be found in 1 Iowa libraries.
Derivation and application of a class of generalized impedance boundary conditions. [Part] II /Author: Volakis, John Leonidas,
Publisher: Ann Arbor, MI : Radiation Laboratory, Department of Electrical Engineering and Computer Science, University of Michigan,
Date: [1989] This title can be found in 1 Iowa libraries.
An investigation into the numerical prediction of boundary layer transition using the K.Y. Chien turbulence model /Author: Stephens, Craig Arden,
Publisher: [Place of publication not identified] : [publisher not identified],
Date: 1989. This title can be found in 1 Iowa libraries.
Numerical simulation of boundary layers. Part 3,Author: Spalart, Philippe R.
Publisher: Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center,
Date: [1986] This title can be found in 1 Iowa libraries.
A boundary-layer computational model for predicting the flow and heat transfer in sudden expansions : technical report /Author: Lewis, J. P.
Publisher: Ames, Iowa : Iowa State University College of Engineering,
Date: 1986. This title can be found in 1 Iowa libraries.
Studies on effects of boundary conditions in confined turbulent flow predictions /Author: Nallasamy, M.
Publisher: [Washington D.C.?] : National Aeronautics and Space Administration, Scientific and Technical Information Branch,
Date: 1985. This title can be found in 1 Iowa libraries.
Scaling and modeling of three-dimensional, end-wall, turbulent boundary layers /Author: Goldberg, Uriel C.
Publisher: [Washington, D.C.?] : National Aeronautics and Space Administration, Scientific and Technical Information Branch,
Date: 1984. This title can be found in 1 Iowa libraries.
Embedded cavity drag in steady and unsteady flows /Author: Gatski, T. B.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center,
Date: [1983] This title can be found in 1 Iowa libraries.
Computer program for solving laminar, transitional, or turbulent compressible boundary-layer equations for two-dimensional and axisymmetric flow /Author: Harris, Julius E.
Publisher: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch,
Date: 1982. This title can be found in 1 Iowa libraries.
Amplified crossflow disturbances in the laminar boundary layer on swept wings with suctionFormat: [microform] /
Author: Dagenhart, J. Ray.
Publisher: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ;
Date: 1981. This title can be found in 1 Iowa libraries.
A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation /Author: Barnwell, Richard W.
Publisher: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch,
Date: 1981. This title can be found in 1 Iowa libraries.
On the effect of boundary layer growth on the stability of compressible flows /Author: El-Hady, Nabil M.
Publisher: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch,
Date: 1981. This title can be found in 1 Iowa libraries.
Viscous-inviscid calculations of jet entrainment effects on the subconic flow over nozzle afterbodies / /c Richard G. WilmothFormat: [microform].
Author: Wilmoth, Richard G.
Publisher: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ;
Date: 1980. This title can be found in 1 Iowa libraries.
A computational model for the prediction of jet entrainment in the vicinity of nozzle boattails (The BOAT code) /Author: Dash, Sanford M.
Publisher: [Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Service,
Date: 1978. This title can be found in 1 Iowa libraries.
Turbulent modeling of a vortex boundary layer flow /Author: Hsu, C. T.
Publisher: Ames, Iowa : Iowa State University College of Engineering,
Date: 1976. This title can be found in 1 Iowa libraries.
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