01099nam0-2200301---450-99000840804040332120061026112454.0000840804FED01000840804(Aleph)000840804FED0100084080420061026d1947----km-y0itay50------baengGBaf------001yy<<The >>effect of spanwise rib-boom stiffness on the stress distribution near a wing cut-outby E. H. MansfieldLondon[s.n.]194716 p., [9] p. di tav.ill.33 cmReports and memorandaAeronautical Research Council, London. Procurement Executive, Ministry of Defense2663In testa al front.: Royal Aircraft establishment, Farnborough. - Report Structures 13Mansfield,Eric Harold298597ITUNINARICAUNIMARCBK990008408040403321A 39DINPADINPAEffect of spanwise rib-boom stiffness on the stress distribution near a wing cut-out725224UNINA