Question: In order to computationally simulate the 2D flow field in a supersonic inlet as shown in the figure below, briefly describe with a suitable
In order to computationally simulate the 2D flow field in a supersonic inlet as shown in the figure below, briefly describe with a suitable sketch the possible fluid domain that can be adopted for the simulation. Mention the different artificial boundaries that will be needed to define the domain boundaries and also describe briefly each artificial boundary adopted. Flow to simulate Flow to simulate 0 Flow to simulate What do you mean by Euler equation? Derive Euler equation. Parts of inlet (Ramp & Cowl)
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