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NASA NTRS · 19860056985

Transonic potential flow in hyperbolic nozzles

Abstract

The full potential equation for the classical problem of transonic flow through a hyperbolic nozzle (with or without a shock wave) is solved in conservation form using the finite volume method of Jameson and Caughey (1977). Either a firstor a second-order numerical viscosity is added in the direction of the flow, explicitly, in conservation form. A multigrid alternating direction implicit method is used to solve the difference equations, and the results obtained are compared with analytical and numerical results from previous researches.

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BibTeXRIS

Park, M., Caughey, D. A.. 1986-06-01. Transonic potential flow in hyperbolic nozzles. https://ntrs.nasa.gov/citations/19860056985

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