NASA NTRS · 19860037943
Numerical solution of 2-D thrust reversing and thrust vectoring nozzle
Abstract
The flowfield within and around two dimensional thrust reversing and thrust vectoring nozzles has been calculated using a new unfactored implicit method with a multiple zone grid. Computations are done for fully deployed thrust reversing nozzles, partially deployed thrust reversing nozzles with thrust vectoring, and a nozzle transitioning from partially to fully deployed. Agreement with available experimental data is good.
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Imlay, S.. 1986-01-01. Numerical solution of 2-D thrust reversing and thrust vectoring nozzle. https://ntrs.nasa.gov/citations/19860037943
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