LEADER 02746oam  2200697I  450 
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035   $a(CKB)5470000002504112
035   $a(OCoLC)1100474462
035   $a(EXLCZ)995470000002504112
100   $a20190508d1950      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAerodynamic characteristics at Reynolds numbers of 3.0 x 10? and 6.0 x 10? of three airfoil sections formed by cutting off various amounts from the rear portion of the NACA 0012 airfoil section /$fby Hamilton A. Smith and Raymond F. Schaefer
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1950.
215   $a1 online resource (18 pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 2074
300   $a"April 1950."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 9).
517 3 $aAerodynamic characteristics at Reynolds numbers of 3.0 x 10(exp 6) and 6.0 x 10(exp 6) of three airfoil sections formed by cutting off various amounts from the rear portion of the National Advisory Committee for Aeronautics 0012 airfoil section
606   $aAerofoils
606   $aAerodynamics
606   $aLift (Aerodynamics)
606   $aDrag (Aerodynamics)
606   $aPitching (Aerodynamics)
606   $aReynolds number
606   $aAerodynamics$2fast
606   $aAerofoils$2fast
606   $aDrag (Aerodynamics)$2fast
606   $aLift (Aerodynamics)$2fast
606   $aPitching (Aerodynamics)$2fast
606   $aReynolds number$2fast
615  0$aAerofoils.
615  0$aAerodynamics.
615  0$aLift (Aerodynamics)
615  0$aDrag (Aerodynamics)
615  0$aPitching (Aerodynamics)
615  0$aReynolds number.
615  7$aAerodynamics.
615  7$aAerofoils.
615  7$aDrag (Aerodynamics)
615  7$aLift (Aerodynamics)
615  7$aPitching (Aerodynamics)
615  7$aReynolds number.
700   $aSmith$b Hamilton A.$01401175
702   $aSchaefer$b Raymond F.
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   $a9910713757103321
996   $aAerodynamic characteristics at Reynolds numbers of 3.0 x 10? and 6.0 x 10? of three airfoil sections formed by cutting off various amounts from the rear portion of the NACA 0012 airfoil section$93469532
997   $aUNINA