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005 20201113143306.0
035   $a(CKB)5470000002507160
035   $a(OCoLC)1136490319
035   $a(EXLCZ)995470000002507160
100   $a20200116d1930      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aSpan load distribution on two monoplane wing models as affected by twist and sweepback /$fby Montgomery Knight and Richard W. Noyes
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1930.
215   $a1 online resource (7 pages, 12 unnumbered pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 346
300   $a"July, 1930."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 5).
606   $aAirplanes$xModels$xWings
606   $aLoads (Mechanics)
606   $aStability of airplanes
606   $aAirplanes$xModels$xWings$2fast
606   $aLoads (Mechanics)$2fast
606   $aStability of airplanes$2fast
615  0$aAirplanes$xModels$xWings.
615  0$aLoads (Mechanics)
615  0$aStability of airplanes.
615  7$aAirplanes$xModels$xWings.
615  7$aLoads (Mechanics)
615  7$aStability of airplanes.
700   $aKnight$b Montgomery$01390967
702   $aNoyes$b Richard W.
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   $a9910714048703321
996   $aSpan load distribution on two monoplane wing models as affected by twist and sweepback$93487447
997   $aUNINA