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Analysis and design of flight vehicle structures E. F. Bruhn

Por: Tipo de material: Archivo de ordenadorArchivo de ordenadorDetalles de publicación: [Carmel] JacobsEdición: [2nd?] edDescripción: ca. 950 p. il. byn, cuadros, gráficos, tablas
Contenidos:
The work of the aerospace structures engineer
Equilibrium of force systems. Truss structures. Externally braced wings. Landing gear
Properties of sections. Centroids, moments of inertia, etc.
General loads on aircraft
Beams. Shear and moments. Beam. Column moments
Torsion. Stresses and deflections
Deflections of structures. Castigliano's theorem. Virtual work. Matrix methods
Statically indeterminate structures. Theorem of least work. Virtual work. Matrix methods
Bending moments in frames and rings by elastic center method
Column analogy method
Continuous structures. Moment distribution method
Slope deflection method
Bending stresses
Bending shear stresses. Solid and open section. Shear center
Shear flow in closed thinwalled sections
Membrane stresses in preasure vessels
Bending of plates
Theory of the instability of columns and thin sheets
Introduction to wing stress analysis by modified beam theory
Introduction to fuselage stress analysis by modified beam theory
Loads and stresses on ribs and frames
Analysis of special wing problems. Cutouts. Shear lag. Swept wing
Analysis by the "Method of displacement"
The 3Dimensional equations of thermoelasticity
The 2Dimensional equations of elasticity and thermoelasticity
Selected problems in elasticity and thermoelasticity
Basic principles and definitions [In flight vehicle materials and their properties]
Mechanical and physical properties of metallic materials for flight vehicle structures
Combined stresses. Theory of yield and ultimate failure
Strength of columns with stable cross sections
Yield and ultimate strength in bending
Strength and design of round, streamline, oval and square tubing in tension, compression, bending, torsion and combined loadings
Buckling strength of flat sheet in compression. Shear, bending and under combined stress systems
Local buckling stress for composite shapes
Crippling strength of composite shapes and sheetstifenner panels in compression. Column strength
Buckling strength of monocoque cylinders
Buckling strength of curved sheet panels and spherical plates. Ultimate strength of stiffened curved sheet structures
Design of metal beams. Web shear resistant (Nonbuckling) type. Part 1 : Flat sheet web with vertical stiffeners. Part 2 : Other types of nonbuckling webs
Diagonal semitension field design. Part 1 : Beams with flat webs. Part 2 : Curved web systems
Sandwich construction and design
Fatigue
Fittings and connections. bolted and riveted
Welded connections
Some important details in structural design
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Libro Libro Biblioteca Dr. Jorge S. Muntaner Coll 629.73.015=111 BRU (Navegar estantería(Abre debajo)) Disponible 010370
Libro Libro Biblioteca Dr. Jorge S. Muntaner Coll 629.73.015=111 BRU (Navegar estantería(Abre debajo)) Disponible 002807
Libro Libro Biblioteca Dr. Jorge S. Muntaner Coll 629.73.015=111 BRU (Navegar estantería(Abre debajo)) Disponible 002808
Libro Libro Biblioteca Dr. Jorge S. Muntaner Coll 629.73.015=111 BRU (Navegar estantería(Abre debajo)) Disponible 004072

Paginación por capítulos

The work of the aerospace structures engineer

Equilibrium of force systems. Truss structures. Externally braced wings. Landing gear

Properties of sections. Centroids, moments of inertia, etc.

General loads on aircraft

Beams. Shear and moments. Beam. Column moments

Torsion. Stresses and deflections

Deflections of structures. Castigliano's theorem. Virtual work. Matrix methods

Statically indeterminate structures. Theorem of least work. Virtual work. Matrix methods

Bending moments in frames and rings by elastic center method

Column analogy method

Continuous structures. Moment distribution method

Slope deflection method

Bending stresses

Bending shear stresses. Solid and open section. Shear center

Shear flow in closed thinwalled sections

Membrane stresses in preasure vessels

Bending of plates

Theory of the instability of columns and thin sheets

Introduction to wing stress analysis by modified beam theory

Introduction to fuselage stress analysis by modified beam theory

Loads and stresses on ribs and frames

Analysis of special wing problems. Cutouts. Shear lag. Swept wing

Analysis by the "Method of displacement"

The 3Dimensional equations of thermoelasticity

The 2Dimensional equations of elasticity and thermoelasticity

Selected problems in elasticity and thermoelasticity

Basic principles and definitions [In flight vehicle materials and their properties]

Mechanical and physical properties of metallic materials for flight vehicle structures

Combined stresses. Theory of yield and ultimate failure

Strength of columns with stable cross sections

Yield and ultimate strength in bending

Strength and design of round, streamline, oval and square tubing in tension, compression, bending, torsion and combined loadings

Buckling strength of flat sheet in compression. Shear, bending and under combined stress systems

Local buckling stress for composite shapes

Crippling strength of composite shapes and sheetstifenner panels in compression. Column strength

Buckling strength of monocoque cylinders

Buckling strength of curved sheet panels and spherical plates. Ultimate strength of stiffened curved sheet structures

Design of metal beams. Web shear resistant (Nonbuckling) type. Part 1 : Flat sheet web with vertical stiffeners. Part 2 : Other types of nonbuckling webs

Diagonal semitension field design. Part 1 : Beams with flat webs. Part 2 : Curved web systems

Sandwich construction and design

Fatigue

Fittings and connections. bolted and riveted

Welded connections

Some important details in structural design

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