ereprof. ir. Erik Dick
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An algebraic transition model combined with the k-ω RANS model for turbomachinery use
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An algebraic model for bypass transition in turbomachinery boundary layer flows
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Solving low Mach number Riemann problems by a momentum interpolation method
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Fundamentals of turbomachines
(2015) -
An algebraic intermittency model added to the k-omega RANS model for transition simulation
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Godunov-type schemes with an inertia term for unsteady full Mach number range flow calculations
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Momentum interpolation for quasi one-dimensional unsteady low Mach number flows with acoustics
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- Conference Paper
- C3
- open access
Inertia terms for all Mach number Godunov-type schemes: behavior of unsteady solutions al low Mach number
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Solving low mach number Riemann problems by momentum interpolation
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Residual stress reconstruction for large-Eddy simulation