LEADER 02175oam  2200625I  450 
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035   $a(CKB)5470000002503171
035   $a(OCoLC)1100474465
035   $a(EXLCZ)995470000002503171
100   $a20190508d1932      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe aerodynamic characteristics of a model wing having a split flap deflected downward and moved to the rear /$fby Fred E. Weick and Thomas A. Harris
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1932.
215   $a1 online resource (7 pages, 11 unnumbered pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 422
300   $a"May, 1932."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 6).
606   $aWind tunnel testing
606   $aSplit flaps (Airplanes)
606   $aAirplanes$xModels$xWings
606   $aTrailing edge flaps
606   $aTrailing edge flaps$2fast
606   $aAirplanes$xModels$xWings$2fast
606   $aSplit flaps (Airplanes)$2fast
606   $aWind tunnel testing$2fast
615  0$aWind tunnel testing.
615  0$aSplit flaps (Airplanes)
615  0$aAirplanes$xModels$xWings.
615  0$aTrailing edge flaps.
615  7$aTrailing edge flaps.
615  7$aAirplanes$xModels$xWings.
615  7$aSplit flaps (Airplanes)
615  7$aWind tunnel testing.
700   $aWeick$b Fred E.$01387817
702   $aHarris$b Thomas A.
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
801  2$bMUB
801  2$bOCL
801  2$bGPO
906   $aBOOK
912   $a9910713650303321
996   $aThe aerodynamic characteristics of a model wing having a split flap deflected downward and moved to the rear$93476038
997   $aUNINA