NASA NTRS · 19810036796
Supersonic viscous flow over cones at incidence
Abstract
The conically symmetric Navier-Stokes equations are solved by MacCormack's method for the supersonic flow past sharp cones at incidence. To provide closure for the case of turbulent flows, a scalar eddy-viscosity model based on mixing length hypotheses is used. The results are compared with available experimental data.
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Mcrae, D. S., Hussaini, M. Y.. 1979-01-01. Supersonic viscous flow over cones at incidence. https://ntrs.nasa.gov/citations/19810036796
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