LEADER 01938oam  2200517I  450 
001 9910707007803321
005 20160406123325.0
035   $a(CKB)5470000002461414
035   $a(OCoLC)703662848
035   $a(EXLCZ)995470000002461414
100   $a20110224j199704    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aInlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ° angle of attack /$fKevin R. Walsh [and three others]
210  1$aEdwards, California.:$cNational Aeronautics and Space Administration, Dryden Flight Research Center,$dApril 1997.
215   $a1 online resource (45 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v104329
300   $aTitle from title screen (viewed April 6, 2016).
300   $a"April 1997."
300   $a"Performing organization: Analytical Services & Materials, Inc. [and] General Electric Aircraft Engines"--Report documentation page.
320   $aIncludes bibliographical references (pages 26-27).
606   $aF-18 aircraft$2nasat
606   $aAngle of attack$2nasat
606   $aAerodynamic characteristics$2nasat
606   $aPressure recovery$2nasat
606   $aEngine inlets$2nasat
615  7$aF-18 aircraft.
615  7$aAngle of attack.
615  7$aAerodynamic characteristics.
615  7$aPressure recovery.
615  7$aEngine inlets.
700   $aWalsh$b Kevin R.$0223814
712 02$aAnalytical Services & Materials, Inc.
712 02$aGE Aircraft Engines (Firm)
712 02$aNASA Dryden Flight Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bSSN
801  1$bSSN
801  2$bGPO
906   $aBOOK
912   $a9910707007803321
996   $aInlet distortion for an F$93547666
997   $aUNINA