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100   $a20190508d1949      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAerodynamic characteristics of 15 NACA airfoil sections at seven Reynolds numbers from 0.7 x 10? to 9.0 x 10? /$fby Laurence K. Loftin, Jr. and Hamilton A. Smith
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1949.
215   $a1 online resource (75 pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 1945
300   $a"October 1949."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 17).
517 3 $aAerodynamic characteristics of fifteen National Advisory Committee for Aeronautics airfoil sections at seven Reynolds numbers from 0.7 x 10(exp 6) to 9.0 x 10(exp 6)
606   $aAerofoils
606   $aAerodynamics
606   $aReynolds number
606   $aAerodynamics$2fast
606   $aAerofoils$2fast
606   $aReynolds number$2fast
606   $aAerodynamic characteristics$2nasat
606   $aAirfoil profiles$2nasat
615  0$aAerofoils.
615  0$aAerodynamics.
615  0$aReynolds number.
615  7$aAerodynamics.
615  7$aAerofoils.
615  7$aReynolds number.
615  7$aAerodynamic characteristics.
615  7$aAirfoil profiles.
700   $aLoftin$b Laurence K.$01398356
702   $aSmith$b Hamilton A.
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   $a9910713762603321
996   $aAerodynamic characteristics of 15 NACA airfoil sections at seven Reynolds numbers from 0.7 x 10? to 9.0 x 10?$93462005
997   $aUNINA