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005 20210427123317.0
035   $a(CKB)5470000002517084
035   $a(OCoLC)1145760021
035   $a(EXLCZ)995470000002517084
100   $a20200323d1935      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aCalculations of the effect of wing twist on the air forces acting on a monoplane wing /$fby G. Da?twyler
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1935.
215   $a1 online resource (17 pages, 10 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 520
300   $a"March 1935."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 17).
606   $aAirplanes$xWings
606   $aAeronautics$xResearch
606   $aAeronautics$xResearch$2fast
606   $aAirplanes$xWings$2fast
615  0$aAirplanes$xWings.
615  0$aAeronautics$xResearch.
615  7$aAeronautics$xResearch.
615  7$aAirplanes$xWings.
700   $aDatwyler$b G.$01405898
712 02$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   $a9910715901603321
996   $aCalculations of the effect of wing twist on the air forces acting on a monoplane wing$93483329
997   $aUNINA