LEADER 01882oam  2200529I  450 
001 9910713976503321
005 20201001141700.0
035   $a(CKB)5470000002505895
035   $a(OCoLC)1136490294
035   $a(EXLCZ)995470000002505895
100   $a20200116d1930      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe effect of wing tip floating ailerons on the autorotation of a monoplane wing model /$fby Montgomery Knight and Carl J. Wenzinger
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1930.
215   $a1 online resource (19 pages, 6 unnumbered pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 336
300   $a"March, 1930."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 13).
606   $aAilerons
606   $aFlaps (Airplanes)
606   $aRolling (Aerodynamics)
606   $aWind tunnel testing
606   $aRolling (Aerodynamics)$2fast
606   $aWind tunnel testing$2fast
615  0$aAilerons.
615  0$aFlaps (Airplanes)
615  0$aRolling (Aerodynamics)
615  0$aWind tunnel testing.
615  7$aRolling (Aerodynamics)
615  7$aWind tunnel testing.
700   $aKnight$b Montgomery$01390967
702   $aWenzinger$b Carl J$g(Carl Joseph),$f1903-1988,
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   $a9910713976503321
996   $aThe effect of wing tip floating ailerons on the autorotation of a monoplane wing model$93446722
997   $aUNINA