LEADER 01932oam  2200565   450 
001 9910716721103321
005 20210831134942.0
035   $a(CKB)5470000002524968
035   $a(OCoLC)1159597638
035   $a(EXLCZ)995470000002524968
100   $a20200623d1937      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aPressure distribution over a Clark Y-H airfoil section with a split flap /$fby Carl J. Wenzinger
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1937.
215   $a1 online resource (5 pages, 6 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 627
300   $a"December 1937."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 5).
606   $aAerofoils
606   $aSplit flaps (Airplanes)
606   $aAerodynamic load
606   $aWind tunnel testing
606   $aAerodynamic load$2fast
606   $aAerofoils$2fast
606   $aSplit flaps (Airplanes)$2fast
606   $aWind tunnel testing$2fast
615  0$aAerofoils.
615  0$aSplit flaps (Airplanes)
615  0$aAerodynamic load.
615  0$aWind tunnel testing.
615  7$aAerodynamic load.
615  7$aAerofoils.
615  7$aSplit flaps (Airplanes)
615  7$aWind tunnel testing.
700   $aWenzinger$b Carl J$g(Carl Joseph),$f1903-1988,$01386955
712 02$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   $a9910716721103321
996   $aPressure distribution over a Clark Y-H airfoil section with a split flap$93459782
997   $aUNINA