Pages that link to "Item:Q1626355"
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The following pages link to A characteristic inlet boundary condition for compressible, turbulent, multispecies turbomachinery flows (Q1626355):
Displaying 13 items.
- Implementation of synthetic turbulence inlet for turbomachinery LES (Q536768) (← links)
- Improved model to determine turbine and compressor boundary conditions with the method of characteristics (Q986355) (← links)
- On the importance of inlet boundary conditions for aerothermal predictions of turbine stages with large eddy simulation (Q1648371) (← links)
- A mesh adaptation strategy for complex wall-modeled turbomachinery LES (Q2028136) (← links)
- Strong compact formalism for characteristic boundary conditions with discontinuous spectral methods (Q2123344) (← links)
- Inlet boundary conditions for incompressible LES: a comparative study (Q2256460) (← links)
- Flow and performance characteristics of twin-entry radial turbine under full and extreme partial admission conditions (Q2267949) (← links)
- Boundary condition optimization to improve the stability of inviscid and compressible finite-volume methods on unstructured meshes (Q2294021) (← links)
- A generalized non-reflecting inlet boundary condition for steady and forced compressible flows with injection of vortical and acoustic waves (Q2313691) (← links)
- Assessment of inflow boundary conditions for compressible turbulent boundary layers (Q3554521) (← links)
- Development and validation of Navier-Stokes characteristic boundary conditions applied to turbomachinery simulations using the lattice Boltzmann method (Q6537432) (← links)
- A polynomial-correction Navier-Stokes characteristic boundary condition (Q6592731) (← links)
- Two-phase magma flow with phase exchange: Part I. Physical modeling of a volcanic conduit (Q6670568) (← links)
