01923oam 2200529I 450 991071336650332120200330141611.0(CKB)5470000002499977(OCoLC)1111633652(EXLCZ)99547000000249997720190806d1922 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierThe effect of longitudinal moment of inertia upon dynamic stability /by F.H. Norton and T. Carroll[Washington, D.C.] :National Advisory Committee for Aeronautics,1922.1 online resource (3 pages, 1 unnumbered page) illustrationTechnical notes / National Advisory Committee for Aeronautics ;No. 115"October, 1922."No Federal Depository Library Program (FDLP) item number.Includes bibliographical reference (page 1).Stability of airplanesStability of airplanes, LongitudinalMoments of inertiaMoments of inertiafastStability of airplanesfastStability of airplanes, LongitudinalfastStability of airplanes.Stability of airplanes, Longitudinal.Moments of inertia.Moments of inertia.Stability of airplanes.Stability of airplanes, Longitudinal.Norton F. H(Frederick Harwood),1896-1992,18769Carroll ThomasUnited States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCFOCLCOGPOBOOK9910713366503321The effect of longitudinal moment of inertia upon dynamic stability3466596UNINA