LEADER 02153oam  2200625   450 
001 9910716874003321
005 20210921141936.0
035   $a(CKB)5470000002525444
035   $a(OCoLC)1159597665
035   $a(EXLCZ)995470000002525444
100   $a20200623d1938      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aWind-tunnel tests of a Clark Y wing having split flaps with gaps /$fby Carl J. Wenzinger
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1938.
215   $a1 online resource (4 pages, 3 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 650
300   $a"May 1938."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 4).
606   $aAirplanes$xModels$xWings
606   $aSplit flaps (Airplanes)
606   $aLift (Aerodynamics)
606   $aDrag (Aerodynamics)
606   $aWind tunnel testing
606   $aAirplanes$xModels$xWings$2fast
606   $aDrag (Aerodynamics)$2fast
606   $aLift (Aerodynamics)$2fast
606   $aSplit flaps (Airplanes)$2fast
606   $aWind tunnel testing$2fast
615  0$aAirplanes$xModels$xWings.
615  0$aSplit flaps (Airplanes)
615  0$aLift (Aerodynamics)
615  0$aDrag (Aerodynamics)
615  0$aWind tunnel testing.
615  7$aAirplanes$xModels$xWings.
615  7$aDrag (Aerodynamics)
615  7$aLift (Aerodynamics)
615  7$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$bTRAAL
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910716874003321
996   $aWind-tunnel tests of a Clark Y wing having split flaps with gaps$93459727
997   $aUNINA