I have considerable interest in the application of machine learning techniques to (computational) fluid dynamics. I’ll collect the related information and enhance the following links.
the existence of objects: free jet and impinging jet
the differences of physical properties between a projected fluid and an ambient fluid: submerged jet and unsubmerged jet
the geometry of a nozzle: round jet and slot jet
and so on.
Free Jet
The following video visualizes the flow pattern of a submerged free jet (created by Bjarke Ove Andersen and Mathies Hjorth Jensen of Technical University of Denmark):
Flow Regions of Impinging Jet [1, 2]
Region Ⅰ is the region of flow establishment. It extends from the nozzle exit to the apex of the potential core. The so-called potential core is the central portion of the flow in which the velocity remains constant and equal to the velocity at the nozzle exit.
Region Ⅱ is a region of established flow in the direction of the jet beyond the apex of the potential core; it is characterized by a dissipation of the centerline jet velocity and by a spreading of the jet in the transverse direction.
Region Ⅲ is that region in which the jet is deflected from the axial direction.
Region Ⅳ is known as the wall jet region, where the directed flow increases in thickness as the boundary layer builds up along the solid surface.
I’ve looked for some benchmark problems in the computational aeroacoustics (CAA) and found the eight problem categories that the BANC (Benchmark Problems for Airframe Noise Computations) workshop has addressed. This workshop is sponsored by the Aeroacoustics Technical Committee.