LEADER 01911oam  2200565   450 
001 9910713416403321
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035   $a(CKB)5470000002501493
035   $a(OCoLC)1121049808
035   $a(EXLCZ)995470000002501493
100   $a20190926d1924      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe induction factor used for computing the rolling moment due to the ailerons /$fby Max M. Munk
210  1$a[Washington, D.C.] :$cNational Advisory Committee for Aeronautics,$d1924.
215   $a1 online resource (4 pages, 1 unnumbered page) $cillustration
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 187
300   $a"April, 1924."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 1).
606   $aAilerons
606   $aRolling (Aerodynamics)
606   $aFlaps (Airplanes)
606   $aAerodynamics
606   $aMathematical models
606   $aAerodynamics$2fast
606   $aMathematical models$2fast
606   $aRolling (Aerodynamics)$2fast
615  0$aAilerons.
615  0$aRolling (Aerodynamics)
615  0$aFlaps (Airplanes)
615  0$aAerodynamics.
615  0$aMathematical models.
615  7$aAerodynamics.
615  7$aMathematical models.
615  7$aRolling (Aerodynamics)
700   $aMunk$b Max M$g(Max Michael),$f1890-$01386130
712 02$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   $a9910713416403321
996   $aThe induction factor used for computing the rolling moment due to the ailerons$93526001
997   $aUNINA