000			01736mm a2200445a 44500
001			NM002996
003			AR-HaUTN
005			20240912182206.0
007			ta
008			12020sc. 1 ||||||||||||||000 | spa||
040			_aAR-HaUTN _cAR-HaUTN
100			_aShanley, F. R. _93189
245			_aWeigh-tstrength analysis of aircraft structures _cF. R. Shanley
250			_a2nd ed.
260			_aNew York _bDover
300			_a404 p. _bgráficos
500			_aIndice alfabético, al final del libro
504			_aReferencias bibliográficas p. 387396
505			_tMethods of analysis
505			_tPrinciples of structural design for minimun weight
505			_tGeneral instability of stiffenes shells in pure bending
505			_tMinimun weight of stiffened cylindrical shells in pure bending
505			_tEffect of torsionalstiffness requirements on wing structural weight
505			_tGeneral weightanalysis methods
505			_tWieght analysis of the sheetstringerrib type of wing structure
505			_tEffective depth of airfoil sections
505			_tEvaluation of integration factors
505			_tInertia and shear reduction factors
505			_tWing ribs and secondary structure
505			_tNon optimum structural weight
505			_tWeight analysis of the thickplate type of wing structure
505			_tWeight analysis of thinwing structures
505			_tWeight analysis of fuselage and shell structures
505			_tAnalysis of stressstraintime relations
505			_tStressstraintime properties of same aircraft materials
505			_tInelastic column theory
505			_tPrinciples of creep buckling
505			_tEffect of creep on column deflection
942			_cBK _2udc
999			_c2996 _d2996