Stall analysis in a transonic compressor stage and rotor
Approved for public release; distribution is unlimited === Gas turbine engine design is based on simplifying assumptions, including axi-symmetric flow. These assumptions break down in the real machines especially when operating near to stall. The reduction in operating surge margin associated with...
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Monterey, California. Naval Postgraduate School
2012
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| Online Access: | http://hdl.handle.net/10945/4749 |