TRANSITION MODELLING BASED ON LOCAL VARIABLES
By F. Menter, Thomas Esch, S. Kubacki. 2002
177 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computational Mechanics
View Paper: https://www.semanticscholar.org/paper/f843407bd89432c8e820865d5e8d42bae30ddb9c
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In Aerospace Engineering
In Computational Mechanics
Citations in the corpus
- A correlation-based transition model using local variables for unstructured parallelized CFD codes (2011, methodology): “…the maximum of the profile is proportional to the momentum thickness Reynolds number and can therefore be related to the transition correlations (Menter et al., 2002) as follows: ( ) 193.2 RemaxRe v=θ (3.2) Based on this observation, a general framework can be built, which can serve as a local…”
- Correlation-Based Transition Modeling for Unstructured Parallelized Computational Fluid Dynamics Codes (2009, methodology): “[22].”
- Computational Fluid Dynamics Compatible Transition Modeling Using an Amplification Factor Transport Equation (2014, methodology): “[9] and more fully developed by Langtry andMenter [10], which locally evaluates a transition criterion in a manner that is fully compatible with modern CFD solvers.”
- Transition Modelling for General Purpose CFD Codes (2006, methodology): “Instead of using the momentum thickness Reynolds number to trigger the onset of transition, the current model is based on the strain-rate (or vorticity) Reynolds number, Rev, [15, 35]:”
- Heat transfer in all pipe flow regimes: laminar, transitional/intermittent, and turbulent (2009, background): “The most current and readily implemented scheme for predicting transition and skin friction in external flows is that formulated by Menter and co-workers [14–16].”