Preliminary design study of an enhanced mixing eductor system for the LHA (R) gas turbine exhaust
Approved for public release, distribution unlimited === A preliminary design study was conducted to determine the geometry for an enhanced mixing eductor system for the Landing, Helicopter Assault Ship Replacement (LHA R) program gas turbine exhaust. A one-dimensional analytical model, with a corr...
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Monterey, California. Naval Postgraduate School
2012
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| Online Access: | http://hdl.handle.net/10945/6210 |