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Wylleman and Lavallee's (2004) developmental model on transitions faced by athletes and Stambulova's (1997, 2003) athletic career transition model were used to provide the theoretical foundation of inquiry.
The XFOIL code, the Shear Stress Transport k−ω turbulence model and a refurbished version of k−kl−ω transition model were used to predict the airfoil aerodynamic performance at low Reynolds numbers (around 2.0×105).
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The transition model is a weighted finite-state transducer (WFST).
The transition model is given by (11) which is a first autoregressive model AR (11).
A state transition model is constructed to model this cognitive operation.
This transition model is represented as a dynamic Bayesian network (DBN).
Constructive approach to a phase transition model was presented in [22].
Computational setup and transition model is described in detail in Sect. 4.
The SST turbulence model coupled with γ-θ transition model is applied for the present simulations.
Due to the moderate Reynolds number, a laminar to turbulent transition model was also activated.
A robust solution procedure for the transition model is described and a grid convergence study is presented.
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