LEADER 02201oam  2200637   450 
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035   $a(CKB)5470000002507844
035   $a(OCoLC)1100474485
035   $a(EXLCZ)995470000002507844
100   $a20190508d1950      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAerodynamic coefficients for an oscillating airfoil with hinged flap, with tables for a Mach number of 0.7 /$fby M. J. Turner and S. Rabinowitz
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1950.
215   $a1 online resource (46 pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 2213
300   $a"October 1950"
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 19).
606   $aAerofoils
606   $aFlaps (Airplanes)
606   $aLift (Aerodynamics)
606   $aPitching (Aerodynamics)
606   $aHinge moments (Aerodynamics)
606   $aAerofoils$2fast
606   $aFlaps (Airplanes)$2fast
606   $aHinge moments (Aerodynamics)$2fast
606   $aLift (Aerodynamics)$2fast
606   $aPitching (Aerodynamics)$2fast
615  0$aAerofoils.
615  0$aFlaps (Airplanes)
615  0$aLift (Aerodynamics)
615  0$aPitching (Aerodynamics)
615  0$aHinge moments (Aerodynamics)
615  7$aAerofoils.
615  7$aFlaps (Airplanes)
615  7$aHinge moments (Aerodynamics)
615  7$aLift (Aerodynamics)
615  7$aPitching (Aerodynamics)
700   $aTurner$b M. J.$01404882
702   $aRabinowitz$b S.
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   $a9910715016403321
996   $aAerodynamic coefficients for an oscillating airfoil with hinged flap, with tables for a Mach number of 0.7$93480367
997   $aUNINA