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101 0 $aeng
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181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 04$aThe effect of modified control limits on the performance of a generic commercial aircraft engine$b[electronic resource] /$fJeffrey T. Csank ... [and others] ; prepared for the 47th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE, San Diego, California, July 31-August 3, 2011
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2012]
215   $a1 online resource (9 pages) $ccolor illustrations
225 1 $aNASA TM- ;$v2012-217261
300   $aTitle from title screen (viewed on Sept. 6, 2012).
300   $a"January 2012."
300   $a"AIAA-2011-5972."
320   $aIncludes bibliographical references (page 9)
606   $aAircraft control$2nasat
606   $aEngine failure$2nasat
606   $aRotors$2nasat
606   $aProbability theory$2nasat
606   $aCommercial aircraft$2nasat
606   $aEmergencies$2nasat
615  7$aAircraft control.
615  7$aEngine failure.
615  7$aRotors.
615  7$aProbability theory.
615  7$aCommercial aircraft.
615  7$aEmergencies.
701   $aCsank$b Jeffrey T$01402819
712 02$aNASA Glenn Research Center.
712 12$aJoint Propulsion Conference and Exhibit$d(47th :$f2011 :$eSan Diego, Calif.)
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