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100   $a20190508d1954      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAerodynamic characteristics of the NACA 64-010 and 0010-1.10 40/1.051 airfoil sections at Mach numbers from 0.30 to 0.85 and Reynolds numbers from 4.0 x 10? to 8.0 x 10? /$fby Laurence K. Loftin, Jr
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1954.
215   $a1 online resource (17 pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 3244
300   $a"August 1954."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 5).
517 3 $aAerodynamic characteristics of the National Advisory Committee for Aeronautics 64-010 and 0010-1.10 40/1.051 airfoil sections at Mach numbers from 0.30 to 0.85 and Reynolds numbers from 4.0 x 10(exp. 6) to 8.0 x 10(exp. 6)
606   $aAerofoils
606   $aAerodynamics
606   $aMach number
606   $aReynolds number
606   $aAerodynamics$2fast
606   $aAerofoils$2fast
606   $aMach number$2fast
606   $aReynolds number$2fast
615  0$aAerofoils.
615  0$aAerodynamics.
615  0$aMach number.
615  0$aReynolds number.
615  7$aAerodynamics.
615  7$aAerofoils.
615  7$aMach number.
615  7$aReynolds number.
700   $aLoftin$b Laurence K.$01398356
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bCOP
801  2$bTRAAL
801  2$bGPO
906   $aBOOK
912   $a9910713887303321
996   $aAerodynamic characteristics of the NACA 64-010 and 0010-1.10 40$93522372
997   $aUNINA