Weigh-tstrength analysis of aircraft structures

Shanley, F. R.

Weigh-tstrength analysis of aircraft structures F. R. Shanley - 2nd ed. - New York Dover - 404 p. gráficos

Indice alfabético, al final del libro

Referencias bibliográficas p. 387396

Methods of analysis Principles of structural design for minimun weight General instability of stiffenes shells in pure bending Minimun weight of stiffened cylindrical shells in pure bending Effect of torsionalstiffness requirements on wing structural weight General weightanalysis methods Wieght analysis of the sheetstringerrib type of wing structure Effective depth of airfoil sections Evaluation of integration factors Inertia and shear reduction factors Wing ribs and secondary structure Non optimum structural weight Weight analysis of the thickplate type of wing structure Weight analysis of thinwing structures Weight analysis of fuselage and shell structures Analysis of stressstraintime relations Stressstraintime properties of same aircraft materials Inelastic column theory Principles of creep buckling Effect of creep on column deflection