LEADER 01923oam  2200529I  450 
001 9910713366503321
005 20200330141611.0
035   $a(CKB)5470000002499977
035   $a(OCoLC)1111633652
035   $a(EXLCZ)995470000002499977
100   $a20190806d1922      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe effect of longitudinal moment of inertia upon dynamic stability /$fby F.H. Norton and T. Carroll
210  1$a[Washington, D.C.] :$cNational Advisory Committee for Aeronautics,$d1922.
215   $a1 online resource (3 pages, 1 unnumbered page) $cillustration
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 115
300   $a"October, 1922."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical reference (page 1).
606   $aStability of airplanes
606   $aStability of airplanes, Longitudinal
606   $aMoments of inertia
606   $aMoments of inertia$2fast
606   $aStability of airplanes$2fast
606   $aStability of airplanes, Longitudinal$2fast
615  0$aStability of airplanes.
615  0$aStability of airplanes, Longitudinal.
615  0$aMoments of inertia.
615  7$aMoments of inertia.
615  7$aStability of airplanes.
615  7$aStability of airplanes, Longitudinal.
700   $aNorton$b F. H$g(Frederick Harwood),$f1896-1992,$018769
702   $aCarroll$b Thomas
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCF
801  2$bOCLCO
801  2$bGPO
906   $aBOOK
912   $a9910713366503321
996   $aThe effect of longitudinal moment of inertia upon dynamic stability$93466596
997   $aUNINA