LEADER 01946oam  2200505I  450 
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035   $a(EXLCZ)995470000002461397
100   $a20110224j199609    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEvaluation of high-angle-of-attack handling qualities for the X-31A using standard evaluation maneuvers /$fPatrick C. Stoliker and John T. Bosworth
210  1$aEdwards, California :$cNational Aeronautics and Space Administration, Dryden Flight Research Center,$dSeptember 1996.
215   $a1 online resource (32 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v104322
300   $aTitle from title screen (viewed April 5, 2016).
300   $a"September 1996."
300   $a"Performing organization: NASA Dryden Flight Research Center, Edwards, California"--Report documentation page.
320   $aIncludes bibliographical references (pages 31-32).
606   $aAircraft maneuvers$2nasat
606   $aAngle of attack$2nasat
606   $aFlight control$2nasat
606   $aPilot induced oscillation$2nasat
606   $aX-31 aircraft$2nasat
615  7$aAircraft maneuvers.
615  7$aAngle of attack.
615  7$aFlight control.
615  7$aPilot induced oscillation.
615  7$aX-31 aircraft.
700   $aStoliker$b P. C.$01389353
702   $aBosworth$b John T.
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   $a9910707009503321
996   $aEvaluation of high-angle-of-attack handling qualities for the X-31A using standard evaluation maneuvers$93440793
997   $aUNINA