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NASA NTRS ยท 19740008900

The computation of steady nozzle flow by a time-dependent method

Abstract

The steady flow in two-dimensional and axisymmetric nozzles was computed using a time-dependent method. In this method the interior mesh points were computed using the MacCormack finite-difference scheme, while a characteristic scheme was used to calculate the boundary mesh points. No explicit artificial viscosity term was included. The fluid was assumed to be a perfect gas. This method was used to compute the flow in a 45 deg - 15 deg conical, converging-diverging nozzle, a 15 deg conical, converging nozzle, and a 10 deg conical, plug nozzle. Good agreement between the numerical solution and experimental data was found. In contrast to previous time-dependent methods, the computational times were less than one minute on a CDC 6600 computer.

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BibTeXRIS

Cline, M. C.. 1974-04-01. The computation of steady nozzle flow by a time-dependent method. https://ntrs.nasa.gov/citations/19740008900

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