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181   $ctxt$2rdacontent
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200 00$aOptical characterization of a multipoint lean direct injector for gas turbine combustors$b[electronic resource] $evelocity and fuel drop size measurements /$fChristopher M. Heath ... [and others] ; prepared for the Turbo Expo 2010 sponsored by the American Society of Mechanical Engineers (ASME), Glasgow, Scotland, United Kingdom, June 14-18, 2010
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2010]
215   $a1 online resource (13 pages) $cillustrations, color
225 1 $aNASA/TM ;$v2010-216365
300   $aTitle from title screen (viewed on April 21, 2011).
300   $a"October 2010."
320   $aIncludes bibliographical references (page 13).
517   $aOptical characterization of a multipoint lean direct injector for gas turbine combustors 
606   $aFuel injection$2nasat
606   $aGas turbines$2nasat
606   $aFlight conditions$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aCombustion chambers$2nasat
606   $aAircraft engines$2nasat
606   $aFlame temperature$2nasat
606   $aInlet temperature$2nasat
606   $aSupersonic flight$2nasat
615  7$aFuel injection.
615  7$aGas turbines.
615  7$aFlight conditions.
615  7$aComputational fluid dynamics.
615  7$aCombustion chambers.
615  7$aAircraft engines.
615  7$aFlame temperature.
615  7$aInlet temperature.
615  7$aSupersonic flight.
701   $aHeath$b Christopher M$01395901
712 02$aNASA Glenn Research Center.
712 12$aASME Turbo Expo$f(2010 :$eGlasgow, Scotland)
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