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035   $a(EXLCZ)995470000002510172
100   $a20200326d1933      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe effect of partial-span split flaps on the aerodynamic characteristics of a Clark Y wing /$fby Carl J. Wenzinger
210  1$aWashington [D.C.] :$cNational Advisory Committee for Aeronautics,$d1933.
215   $a1 online resource (5 pages, 4 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 472
300   $a"September, 1933."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 4).
606   $aAirplanes$xModels$xWings
606   $aWind tunnel testing
606   $aAirplanes$xModels$xWings$2fast
606   $aWind tunnel testing$2fast
615  0$aAirplanes$xModels$xWings.
615  0$aWind tunnel testing.
615  7$aAirplanes$xModels$xWings.
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   $a9910715385903321
996   $aThe effect of partial-span split flaps on the aerodynamic characteristics of a Clark Y wing$93541814
997   $aUNINA