LEADER 01855oam  2200529   450 
001 9910717079703321
005 20211210154034.0
035   $a(CKB)5470000002527406
035   $a(OCoLC)1262900324
035   $a(OCoLC)995470000002527406
035   $a(EXLCZ)995470000002527406
100   $a20210805j194812    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe development of cambered airfoil sections having favorable lift characteristics at supercritical Mach numbers /$fby Donald J. Graham
210  1$aWashington :$cNational Advisory Committee for Aeronautics,$dDecember 1948.
215   $a1 online resource (82 pages) $cillustrations
225 1 $aNational Advisory Committee for Aeronautics technical note ;$v1771
300   $a"December 1948."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 17)
606   $aAirfoils$2nasat
606   $aAircraft stability$2nasat
606   $aAircraft control$2nasat
606   $aAerofoils$2fast
606   $aCamber (Aerofoils)$2fast
606   $aLift (Aerodynamics)$2fast
615  7$aAirfoils.
615  7$aAircraft stability.
615  7$aAircraft control.
615  7$aAerofoils.
615  7$aCamber (Aerofoils)
615  7$aLift (Aerodynamics)
700   $aGraham$b Donald J.$01411134
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910717079703321
996   $aThe development of cambered airfoil sections having favorable lift characteristics at supercritical Mach numbers$93501552
997   $aUNINA