Task 2

flow solution for advanced separate flow nozzles response A : structured grid Navier-Stokes approach

By Kenzajiwsjum D. C.

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Publish Date

2001

Publisher

National Aeronautics and Space Administration, Glenn Research Center,Available from NASA Center for Aerospace Information

Language

eng

Pages

Description:

subjects: Exhaust gases, Quality control, Aeroacoustics, Plumes, Structured grids (Mathematics), Acoustic nozzles