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100   $a20110224j199902    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFactors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft /$fW.G. Steenken [and three others]
210  1$aEdwards, California :$cNational Aeronautics and Space Administration, Dryden Flight Research Center$dFebruary 1999.
215   $a1 online resource (vii, 191 pages) $cillustrations
225 1 $aNASA/TM ;$v1999-206572
300   $a"February 1999."
300   $a"Performing organization: NASA Dryden Flight Research Center"--Report documentation page.
320   $aIncludes bibliographical references (page 34).
606   $aF-18 aircraft$2nasat
606   $aAerodynamic stability$2nasat
606   $aAngle of attack$2nasat
606   $aCompressors$2nasat
606   $aControl surfaces$2nasat
606   $aFlight control$2nasat
606   $aResearch vehicles$2nasat
606   $aRotors$2nasat
606   $aSubsonic speed$2nasat
615  7$aF-18 aircraft.
615  7$aAerodynamic stability.
615  7$aAngle of attack.
615  7$aCompressors.
615  7$aControl surfaces.
615  7$aFlight control.
615  7$aResearch vehicles.
615  7$aRotors.
615  7$aSubsonic speed.
700   $aSteenken$b William G.$01392405
712 02$aDryden Flight Research Facility,
801  0$bSSN
801  1$bSSN
801  2$bGPO
906   $aBOOK
912   $a9910706189103321
996   $aFactors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F$93502513
997   $aUNINA