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035   $a(OCoLC)650350381
035   $a(EXLCZ)995470000002384562
100   $a20100727d2005      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aActive aeroelastic wing aerodynamic model development and validation for a modified F/A-18A airplane$b[electronic resource] /$fCorey G. Diebler, Stephen B. Cumming
210  1$aEdwards, Calif. :$cNational Aeronautics and Space Administration, Dryden Flight Research Center,$d[2005]
215   $a1 online resource (47 pages) $cillustrations
225 1 $aNASA TM- ;$v2005-213668
300   $aTitle from title screen (viewed on July 27, 2010).
300   $a"November 2005."
320   $aIncludes bibliographical references (page 47).
410  0$aNASA technical memorandum ;$v213668.
606   $aF-18 aircraft$2nasat
606   $aAeroelastic research wings$2nasat
606   $aFlight tests$2nasat
606   $aAircraft models$2nasat
615  7$aF-18 aircraft.
615  7$aAeroelastic research wings.
615  7$aFlight tests.
615  7$aAircraft models.
700   $aDiebler$b Corey G$01406798
701   $aCumming$b Stephen B$01390001
712 02$aHugh L. Dryden Flight Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910697034203321
996   $aActive aeroelastic wing aerodynamic model development and validation for a modified F$93486567
997   $aUNINA