LEADER 02270oam  2200661   450 
001 9910716607203321
005 20210728124005.0
035   $a(CKB)5470000002524098
035   $a(OCoLC)1159597586
035   $a(EXLCZ)995470000002524098
100   $a20200623d1937      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aTheoretical span loading and moments of tapered wings produced by aileron deflection /$fby H.A. Pearson
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1937.
215   $a1 online resource (30 pages, 11 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 589
300   $a"January 1937."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (pages 21-22).
606   $aAirplanes$xWings
606   $aAspect ratio (Aerofoils)
606   $aAilerons
606   $aLift (Aerodynamics)
606   $aRolling (Aerodynamics)
606   $aYawing (Aerodynamics)
606   $aAilerons$2fast
606   $aAirplanes$xWings$2fast
606   $aAspect ratio (Aerofoils)$2fast
606   $aLift (Aerodynamics)$2fast
606   $aRolling (Aerodynamics)$2fast
606   $aYawing (Aerodynamics)$2fast
615  0$aAirplanes$xWings.
615  0$aAspect ratio (Aerofoils)
615  0$aAilerons.
615  0$aLift (Aerodynamics)
615  0$aRolling (Aerodynamics)
615  0$aYawing (Aerodynamics)
615  7$aAilerons.
615  7$aAirplanes$xWings.
615  7$aAspect ratio (Aerofoils)
615  7$aLift (Aerodynamics)
615  7$aRolling (Aerodynamics)
615  7$aYawing (Aerodynamics)
700   $aPearson$b Henry A$g(Henry Adolph),$f1906-$01398867
712 02$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   $a9910716607203321
996   $aTheoretical span loading and moments of tapered wings produced by aileron deflection$93508471
997   $aUNINA