Weigh-tstrength analysis of aircraft structures F. R. Shanley
Tipo de material: TextoDetalles de publicación: New York DoverEdición: 2nd edDescripción: 404 p. gráficosTipo de ítem | Biblioteca actual | Signatura topográfica | Estado | Fecha de vencimiento | Código de barras | |
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Libro | Biblioteca Dr. Jorge S. Muntaner Coll | 629.73.013=111 SHA (Navegar estantería(Abre debajo)) | Disponible | 001537 |
Navegando Biblioteca Dr. Jorge S. Muntaner Coll estanterías Cerrar el navegador de estanterías (Oculta el navegador de estanterías)
629.73.01=111 STI The anatomy of the aeroplane | 629.73.01=111 STI The design of the aeroplane | 629.73.01=133.1 ECO Mecanique du vol | 629.73.013=111 SHA Weigh-tstrength analysis of aircraft structures | 629.73.015 GAR Apuntes de aeroelasticidad | 629.73.015 UPM Prácticas de aeroelasticidad | 629.73.015 WEG Los sistemas hiperestáticos en el cálculo de aviones introducción práctica |
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
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