00892nam0-22003011i-450-990000055830403321000005583FED01000005583(Aleph)000005583FED0100000558320011111d--------km-y0itay50------baitay-------001yyWeight-strength analysis of aircraft structuresF. R. Shanley.New YorkMcGraw-Hill book company1952XI, 394 p.ill.24 cm<<The >>RAND seriesAeroplaniStruttureResistenza629.134 1Shanley,Francis Reynolds1839ITUNINARICAUNIMARCBK99000005583040332113 F 04 1220340FINBCFINBCWeight-strength analysis of aircraft structures111851UNINAING01