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- W764989840 abstract "A computer implemented numerical method for predicting the flow in and about an isolated three dimensional jet exhaust nozzle is summarized. The approach is based on an implicit numerical method to solve the unsteady Navier-Stokes equations in a boundary conforming curvilinear coordinate system. Recent improvements to the original numerical algorithm are summarized. Equations are given for evaluating nozzle thrust and discharge coefficient in terms of computed flowfield data. The final formulation of models that are used to simulate flow turbulence effect is presented. Results are presented from numerical experiments to explore the effect of various quantities on the rate of convergence to steady state and on the final flowfield solution. Detailed flowfield predictions for several two and three dimensional nozzle configurations are presented and compared with wind tunnel experimental data." @default.
- W764989840 created "2016-06-24" @default.
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- W764989840 date "1980-10-01" @default.
- W764989840 modified "2023-09-25" @default.
- W764989840 title "Numerical method for predicting flow characteristics and performance of nonaxisymmetric nozzles. Part 2: Applications" @default.
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