Experimental Investigation of Fan Rotor Response to Inlet Swirl Distortion
Next generation aircraft design focuses on highly integrated airframe/engine architectures that exploit advantages in system level efficiency and performance. One such design concept incorporates boundary layer ingestion which locates the turbofan engine inlet near enough to the lifting surface of...
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Virginia Tech
2016
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| Online Access: | http://hdl.handle.net/10919/71323 |