A relaxation method for the solution of rotational transonic nozzle flow
This work was successful in demonstrating the feasibility, accuracy, and importance of including the effects of total pressure gradients in evaluating propulsion nozzle performance. In fact, in the cases considered here inlet flow nonuniformities produced effects greater than those which resulted fr...
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/42932 http://scholar.lib.vt.edu/theses/available/etd-06082010-020207/ |