Some Improvements to the γ−Reθt Transition Model

Author:

Kim Dongyoung1,Ezequiel Martin J.1,Carrica Pablo M.1

Affiliation:

1. The University of Iowa, Iowa City, Iowa 52242

Funder

Office of Naval Research

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference16 articles.

1. SlotnickJ.KhodadoustA.AlonsoJ.DarmofalD.GroppW.LurieE.MavriplisD. “CFD Vision 2030 Study: A Path to Revolutionary Computational Aerosciences,” NASA CR-2014-218178, 2014.

2. SmithA. M. O.GamberoniN. “Transition, Pressure Gradient and Stability Theory,” Douglas Aircraft Co. Rept. ES 26388, Santa Monica, CA, 1956.

3. Van IngenJ. L. “A Suggested Semi-Empirical Method for the Calculation of the Boundary Layer Transition Region,” Technische Hogeschool Delft, Vliegtuigbouwkunde Rept. VTH-74, Delft, The Netherlands, 1956.

4. Modeling of Flow Transition Using an Intermittency Transport Equation

5. TRANSITION MODELLING BASED ON LOCAL VARIABLES

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