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100   $a20110224j199910    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEstimated benefits of variable-geometry wing camber control for transport aircraft /$fAlexander Bolonkin, Glenn B. Gilyard
210  1$aEdwards, California :$cNational Aeronautics and Space Administration, Dryden Flight Research Center,$dOctober 1999.
215   $a1 online resource (v, 40 pages) $cillustrations
225 1 $aNASA/TM ;$v1999-206586
300   $a"October 1999."
300   $a"Performing organization: NASA Dryden Flight Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 18-19).
606   $aWing camber$2nasat
606   $aWind tunnel tests$2nasat
606   $aTransport aircraft$2nasat
606   $aAdaptive control$2nasat
606   $aCambered wings$2nasat
615  7$aWing camber.
615  7$aWind tunnel tests.
615  7$aTransport aircraft.
615  7$aAdaptive control.
615  7$aCambered wings.
700   $aBolonkin$b Alexander$01148258
702   $aGilyard$b Glenn B.
712 02$aDryden Flight Research Facility,
801  0$bSSN
801  1$bSSN
801  2$bGPO
906   $aBOOK
912   $a9910706186803321
996   $aEstimated benefits of variable-geometry wing camber control for transport aircraft$93446818
997   $aUNINA