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I conducted a simulation of compressible channel flow at Re_tau=500 and Ma=1.5. The velocity profile and Reynolds stress are agree well with the results of available literature. But the T_bulk profile…
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RocketPy implements Barrowman's equations for subsonic compressible flow. As more and more flights achieve the supersonic regime, it is crucial that our aerodynamic model stays accurate at such condit…
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I was running a 3D reacting flow case similar to the ODW wedge example. It seems, similar to the conical shock example for the tutorial, the outflow boundary is contaminating the upstream flow field a…
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Playing with other flow simulations such as Solidworks Flow Simulation and other [MATLAB scripts](https://www.mathworks.com/matlabcentral/fileexchange/14682-2-d-nozzle-design/content/nozzle.m) it is a…
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## *Repository Creation Request*
Use this to get your experiment repository created or updated on GitHub under Virtual Labs organization.
1. ### Coordinating Institute: *Indian Institute of Techno…
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The default `controller` with `SSPRK43()` in OrdinaryDiffEq.jl is a `PIController` with effective parameters `beta1 = 0.70, beta2 = -0.40`. However, this controller is not step size control stable. We…
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Hi, I have read your work and from the article I read that you assumed an incompressible flow (M= 0.1-0.3). In your opinion could I train the ANN for a wider range of fligh conditions?
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Last time we spoke we mentioned one criterion to determine whether radiation can affect the hydrodynamics. This condition was that the cooling timescale should be smaller than the dynamical timescale.…
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Luca Giacomelli, Iacopo Carusotto
> We investigate the various physical mechanisms that underlie the dynamical instability of a quantized vortex array at the interface between two counter-propagati…
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Hi, everyone!
# Problem description
I want to use dugksFoam to calculate the low-speed incompressible flow passing a micro-cylinder. I found cases like internal flow problems (only wall boundary …