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100   $a20111114j196810    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAerodynamic characteristics of a parasol-wing--body combination utilizing favorable lift interference at Mach numbers from 3.00 to 4.63 /$fby Odell A. Morris and Robert J. Mack
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dOctober 1968.
215   $a1 online resource (36 pages) $cillustrations
225 1 $aNASA technical note ;$vNASA TN D-4855
300   $a"October 1968."
320   $aIncludes bibliographical references (page 7).
606   $aAirplanes$xWings
606   $aLift (Aerodynamics)
606   $aInterference (Aerodynamics)
606   $aAerodynamics
606   $aAerodynamics$2fast
606   $aAirplanes$xWings$2fast
606   $aInterference (Aerodynamics)$2fast
606   $aLift (Aerodynamics)$2fast
615  0$aAirplanes$xWings.
615  0$aLift (Aerodynamics)
615  0$aInterference (Aerodynamics)
615  0$aAerodynamics.
615  7$aAerodynamics.
615  7$aAirplanes$xWings.
615  7$aInterference (Aerodynamics)
615  7$aLift (Aerodynamics)
700   $aMorris$b Odell A.$01419396
702   $aMack$b Robert J.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aLangley Research Center.
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910714075203321
996   $aAerodynamic characteristics of a parasol-wing--body combination utilizing favorable lift interference at Mach numbers from 3.00 to 4.63$93533695
997   $aUNINA