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035   $a(OCoLC)1100474477
035   $a(EXLCZ)995470000002504834
100   $a20190508d1955      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAerodynamic characteristics of NACA 0012 airfoil section at angles of attack from 0° to 180° /$fby Chris C. Critzos, Harry H. Heyson, and Robert W. Boswinkle, Jr
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1955.
215   $a1 online resource (21 pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 3361
300   $a"January 1955."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (pages 11-12).
517 3 $aAerodynamic characteristics of National Advisory Committee for Aeronautics 0012 airfoil section at angles of attack from 0 degrees to 180 degrees
606   $aAerofoils
606   $aAngle of attack (Aerodynamics)
606   $aLift (Aerodynamics)
606   $aAerofoils$2fast
606   $aAngle of attack (Aerodynamics)$2fast
606   $aLift (Aerodynamics)$2fast
615  0$aAerofoils.
615  0$aAngle of attack (Aerodynamics)
615  0$aLift (Aerodynamics)
615  7$aAerofoils.
615  7$aAngle of attack (Aerodynamics)
615  7$aLift (Aerodynamics)
700   $aCritzos$b Chris C.$01404415
702   $aHeyson$b Harry H.
702   $aBoswinkle$b Robert W.
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   $a9910713885603321
996   $aAerodynamic characteristics of NACA 0012 airfoil section at angles of attack from 0° to 180$93478943
997   $aUNINA