01836oam 2200541 450 991071408700332120201104095050.0(CKB)5470000002506799(OCoLC)785280939(OCoLC)57536347(OCoLC)761376080(EXLCZ)99547000000250679920120408j196903 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierA method for determining the total drag of a pointed body of revolution in supersonic flow with turbulent boundary layer /by Charlie M. Jackson, Jr., and Rudeen S. SmithWashington, D.C. :National Aeronautics and Space Administration,March 1969.1 online resource (65 pages) illustrationsNASA technical note ;TN D-5046"March 1969."Includes bibliographical references (pages 48-49).Drag (Aerodynamics)Boundary layerBoundary layerfastDrag (Aerodynamics)fastDrag (Aerodynamics)Boundary layer.Boundary layer.Drag (Aerodynamics)Jackson Charlie M.1395048Smith-Taylor RudeenUnited States.National Aeronautics and Space Administration,Langley Research Center.OCLCEOCLCEEGMAD#OCLCQOCLCOOCLCFOCLCQCOPGPOBOOK9910714087003321A method for determining the total drag of a pointed body of revolution in supersonic flow with turbulent boundary layer3453013UNINA