Weigh-tstrength analysis of aircraft structures F. R. Shanley
Tipo de material:
Archivo de ordenadorDetalles de publicación: New York DoverEdición: 2nd edDescripción: 404 p. gráficos| Tipo de ítem | Biblioteca actual | Signatura topográfica | Estado | Fecha de vencimiento | Código de barras | |
|---|---|---|---|---|---|---|
Libro
|
Biblioteca Dr. Jorge S. Muntaner Coll | 629.73.013=111 SHA (Navegar estantería(Abre debajo)) | Disponible | 001537 |
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
No hay comentarios en este titulo.