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100   $a20110930j199708    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDynamic ground effect for a cranked arrow wing airplane / Robert E. Curry
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,$dAugust 1997.
215   $a1 online resource (17 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v4799
300   $aTitle from title screen (viewed March 30, 2016).
300   $a"August 1997."
300   $a"Performing organization: NASA Dryden Flight Research Center, Edwards, California"--Report documentation page.
320   $aIncludes bibliographical references (pages 16-17).
606   $aAerodynamic characteristics$2nasat
606   $aFlight tests$2nasat
606   $aSupersonic transports$2nasat
606   $aAerodynamic drag$2nasat
606   $aArrow wings$2nasat
615  7$aAerodynamic characteristics.
615  7$aFlight tests.
615  7$aSupersonic transports.
615  7$aAerodynamic drag.
615  7$aArrow wings.
700   $aCurry$b Robert E.$01412496
712 02$aNASA Dryden Flight Research Center.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Program,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCO
801  2$bGPO
906   $aBOOK
912   $a9910707026803321
996   $aDynamic ground effect for a cranked arrow wing airplane$93506165
997   $aUNINA