TY  - DATA
AU  - Shanley, F. R.
TI  - Weigh-tstrength analysis of aircraft structures
CY  - New York
PB  - Dover
N1  - 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
ER  -