Effects of several geometric parameters on the performance of a multiple nozzle eductor system.

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Authors
Moss, Charles Michael
Subjects
multiple nozzle eductor system
cold flow tests
Advisors
Pucci, Paul F.
Date of Issue
1977-09
Date
Publisher
Monterey, CA; Naval Postgraduate School
Language
en_US
Abstract
Cold flow tests of a four nozzle eductor system were conducted to evaluate the effects of certain geometric parameters on eductor performance. Eductor performance was related to non-dimensional parameters governing the flow phenomenon developed from a one-dimensional analysis of a simple eductor system based on conservation of momentum for an incompressible gas. An experimental correlation of these parameters was developed and used to determine the effects of several geometric parameters on eductor performance. The geometries tested consisted of: two mixing stack lengths , 2 and 3 mixing stack diameters long; varying the distance between the primary nozzle exit plane and the entrance to the mixing stack; and addition of a conical transition to the entrance of the constant cross section part of the mixing stack. Within the range of variables tested, the longer mixing stack with a distance between the primary nozzle exit plane and the entrance to the mixing stack of about 0.5 mixing stack diameters without an entrance transition gave the best overall performance.
Type
Thesis
Description
Prepared for: Naval Ship Research and Development Laboratory Annapolis, Code 2833; work request N00167-76 WR 6-0454.
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NPS Report Number
NPS-69PC77092
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