LEADER 02151oam  2200625I  450 
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035   $a(CKB)5470000002503207
035   $a(OCoLC)1104148288
035   $a(EXLCZ)995470000002503207
100   $a20190610d1934      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAerodynamic rolling and yawing moments produced by floating wing-tip ailerons, as measured by the spinning balance /$fby Millard J. Bamber
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1934.
215   $a1 online resource (8 pages, 3 unnumbered pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 493
300   $a"March 1934"
300   $aNo Federal Depository Library Program (FDLP) item number
320   $aIncludes bibliographical references (page 8)
606   $aAilerons
606   $aAirplanes$xWings
606   $aRolling (Aerodynamics)
606   $aWind tunnel testing
606   $aYawing (Aerodynamics)
606   $aAilerons$2fast
606   $aAirplanes$xWings$2fast
606   $aRolling (Aerodynamics)$2fast
606   $aWind tunnel testing$2fast
606   $aYawing (Aerodynamics)$2fast
615  0$aAilerons.
615  0$aAirplanes$xWings.
615  0$aRolling (Aerodynamics)
615  0$aWind tunnel testing.
615  0$aYawing (Aerodynamics)
615  7$aAilerons.
615  7$aAirplanes$xWings.
615  7$aRolling (Aerodynamics)
615  7$aWind tunnel testing.
615  7$aYawing (Aerodynamics)
700   $aBamber$b M. J.$01386953
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bTRAAL
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910713646703321
996   $aAerodynamic rolling and yawing moments produced by floating wing-tip ailerons, as measured by the spinning balance$93526012
997   $aUNINA