LEADER 01836oam  2200541   450 
001 9910714087003321
005 20201104095050.0
035   $a(CKB)5470000002506799
035   $a(OCoLC)785280939$z(OCoLC)57536347$z(OCoLC)761376080
035   $a(EXLCZ)995470000002506799
100   $a20120408j196903    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA method for determining the total drag of a pointed body of revolution in supersonic flow with turbulent boundary layer /$fby Charlie M. Jackson, Jr., and Rudeen S. Smith
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dMarch 1969.
215   $a1 online resource (65 pages) $cillustrations
225 1 $aNASA technical note ;$vTN D-5046
300   $a"March 1969."
320   $aIncludes bibliographical references (pages 48-49).
606   $aDrag (Aerodynamics)
606   $aBoundary layer
606   $aBoundary layer$2fast
606   $aDrag (Aerodynamics)$2fast
615  0$aDrag (Aerodynamics)
615  0$aBoundary layer.
615  7$aBoundary layer.
615  7$aDrag (Aerodynamics)
700   $aJackson$b Charlie M.$01395048
702   $aSmith-Taylor$b Rudeen
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aLangley Research Center.
801  0$bOCLCE
801  1$bOCLCE
801  2$bEGM
801  2$bAD#
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bCOP
801  2$bGPO
906   $aBOOK
912   $a9910714087003321
996   $aA method for determining the total drag of a pointed body of revolution in supersonic flow with turbulent boundary layer$93453013
997   $aUNINA