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Comparison of thin layer Navier-Stokes and coupled Euler / boundary layer calculations of non-equilibrium hypersonic flowsnt effects are solved for the outer (inviscid) region. The external inviscid bow shock is determined by a shock-fitting procedure. The results of calculations for flow over a hyperboloid at Mach = 25.5 show excellent agreement for the wall coefficients and the normal profiles using the two methods.

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The Economics of Transaction Costs binary shadow maps, we show that neural rendering can localize the object and estimate coarse geometry. Our approach reveals that sparse cues in images can be used to estimate geometry using differentiable volumetric rendering. Moreover, our framework is highly generalizable and can work alongside