What’s New in FieldView 21
FieldView 21 includes several new features and improvements, including a first for a CFD post-processor:
the FieldView Auto Partitioner. […]
FieldView 21 includes several new features and improvements, including a first for a CFD post-processor:
the FieldView Auto Partitioner. […]
This animation compares the use of a static vs. moving aero-dynamic device to control of vortex structures behind an Ahmed body. […]
λ2 isosurface with dilatational contours to examine different stages of transition, from receptivity to turbulence onset. […]
This animation depicts Mach contours from an implicit large-eddy simulation of a fluidic oscillator. […]
Simulated unstart in a rectangular cross-section tunnel at Mach 1.8 Mach contours show upstream propagating shock system with multiple structures associated with boundary layer flow separation. […]
FieldView animation courtesy of Prof. Datta V. Gaitonde, Mech. & Aerosp. Eng., The Ohio State University. […]
A jet-in-supersonic-crossflow calculated in OVERFLOW. The crossflow is Mach 4 and is laminar up to the jet. […]
Streamwise vortex pair behind a simulated cargo aircraft. […]
Surface morphing control of transitional shock-boundary layer interaction at Mach 2. […]
Acoustics of under-expanded Mach 1.5 impinging jet with a lift-plate. […]