LEADER 02191oam  2200613   450 
001 9910715927103321
005 20210420120138.0
035   $a(CKB)5470000002516826
035   $a(OCoLC)1145759821
035   $a(EXLCZ)995470000002516826
100   $a20200323d1934      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe effects of full-span and partial-span split flaps on the aerodynamic characteristics of a tapered wing /$fby Carl J. Wenzinger
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1934.
215   $a1 online resource (6 pages, 5 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 505
300   $a"September 1934."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 6).
606   $aAirplanes$xWings$xTesting
606   $aAerodynamics
606   $aFlaps (Airplanes)
606   $aSplit flaps (Airplanes)
606   $aWind tunnel testing
606   $aAerodynamics$2fast
606   $aAirplanes$xWings$xTesting$2fast
606   $aFlaps (Airplanes)$2fast
606   $aSplit flaps (Airplanes)$2fast
606   $aWind tunnel testing$2fast
615  0$aAirplanes$xWings$xTesting.
615  0$aAerodynamics.
615  0$aFlaps (Airplanes)
615  0$aSplit flaps (Airplanes)
615  0$aWind tunnel testing.
615  7$aAerodynamics.
615  7$aAirplanes$xWings$xTesting.
615  7$aFlaps (Airplanes)
615  7$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   $a9910715927103321
996   $aThe effects of full-span and partial-span split flaps on the aerodynamic characteristics of a tapered wing$93466409
997   $aUNINA