Gallery


Transverse Hydrogen Jet in a Supersonic Crossflow using LES

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Pressure Fluctuations in a Controlled-Diffusion Blade Boundary Layer Using Equilibrium Wall-Modeled LES

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Highly Underexpanded Sonic Jets from a Rounded Nozzle at NP5 = 15 Using LES

Streamwise plane

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Transverse plane

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Supersonic Flow Around a Circular Cylinder at Mach 3 Using Immersed Boundary Method

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