Aircraft Structures for Engineering Students , Seventh Edition [7th Ed] (Instructor's Edu Resource 1 of 2, Instructor's Solution Manual) (Solutions)

Front-Matter_2022_Aircraft-Structures-for-Engineering-Students
	Front Matter
Copyright_2022_Aircraft-Structures-for-Engineering-Students
	Copyright
Dedication_2022_Aircraft-Structures-for-Engineering-Students
	Dedication
Preface-to-the-Seventh-Edition-of-Aircr_2022_Aircraft-Structures-for-Enginee
	Preface to the Seventh Edition of Aircraft Structures
Chapter-1---Basic-elasticity_2022_Aircraft-Structures-for-Engineering-Studen
	Basic elasticity
		Stress
		Notation for forces and stresses
		Equations of equilibrium
		Plane stress
		Boundary conditions
		Determination of stresses on inclined planes
		Principal stresses
		Mohr's circle of stress
		Strain
		Compatibility equations
		Plane strain
		Determination of strains on inclined planes
		Principal strains
		Mohr's circle of strain
		Stress-strain relationships
			Temperature effects
		Experimental measurement of surface strains
		Reference
		Further reading
Chapter-2---Two-dimensional-problems-i_2022_Aircraft-Structures-for-Engineer
	Two-dimensional problems in elasticity
		Two-dimensional problems
		Stress functions
		Inverse and semi-inverse methods
		St. Venant's principle
		Displacements
		Bending of an end-loaded cantilever
		Reference
Chapter-3---Torsion-of-solid-sec_2022_Aircraft-Structures-for-Engineering-St
	Torsion of solid sections
		Prandtl stress function solution
		St. Venant warping function solution
		The membrane analogy
		Torsion of a narrow rectangular strip
		References
Chapter-4---Virtual-work-and-energy_2022_Aircraft-Structures-for-Engineering
	Virtual work and energy methods
		Principle of virtual work
			Principle of virtual work for a particle
			Principle of virtual work for a rigid body
			Virtual work in a deformable body
			Work done by internal force systems
				Axial force
				Shear force
				Bending moment
				Torsion
				Hinges
				Sign of internal virtual work
			Virtual work due to external force systems
			Use of virtual force systems
		Applications of the principle of virtual work
		Reference
Chapter-5---Energy-methods_2022_Aircraft-Structures-for-Engineering-Students
	Energy methods
		Strain energy and complementary energy
		Principle of the stationary value of the total complementary energy
		Application to deflection problems
		Application to the solution of statically indeterminate systems
		Unit load method
		Flexibility method
			Self-straining trusses
		Total potential energy
		Principle of the stationary value of the total potential energy
		Principle of superposition
		Reciprocal theorem
		Temperature effects
		References
		Further reading
Chapter-6---Matrix-methods_2022_Aircraft-Structures-for-Engineering-Students
	Matrix methods
		Notation
		Stiffness matrix for an elastic spring
		Stiffness matrix for two elastic springs in line
		Matrix analysis of pin-jointed frameworks
		Application to statically indeterminate frameworks
		Matrix analysis of space frames
		Stiffness matrix for a uniform beam
		Finite element method for continuum structures
			Stiffness matrix for a beam-element
			Stiffness matrix for a triangular finite element
			Stiffness matrix for a quadrilateral element
		References
		Further reading
Chapter-7---Bending-of-thin-pla_2022_Aircraft-Structures-for-Engineering-Stu
	Bending of thin plates
		Pure bending of thin plates
		Plates subjected to bending and twisting
		Plates subjected to a distributed transverse load
			The simply supported edge
			The built-in edge
			The free edge
		Combined bending and in-plane loading of a thin rectangular plate
		Bending of thin plates having a small initial curvature
		Energy method for the bending of thin plates
			Strain energy produced by bending and twisting
			Potential energy of a transverse load
			Potential energy of in-plane loads
		Further reading
Chapter-8---Columns_2022_Aircraft-Structures-for-Engineering-Students
	Columns
		Euler buckling of columns
		Inelastic buckling
		Effect of initial imperfections
		Stability of beams under transverse and axial loads
		Energy method for the calculation of buckling loads in columns
		Flexural-torsional buckling of thin-walled columns
		References
Chapter-9---Thin-plates_2022_Aircraft-Structures-for-Engineering-Students
	Thin plates
		Buckling of thin plates
		Inelastic buckling of plates
		Experimental determination of the critical load for a flat plate
		Local instability
		Instability of stiffened panels
		Failure stress in plates and stiffened panels
		Tension field beams
			Complete diagonal tension
			Incomplete diagonal tension
			Postbuckling behavior
		References
Chapter-10---Structural-vibrat_2022_Aircraft-Structures-for-Engineering-Stud
	Structural vibration
		Oscillation of mass-spring systems
		Oscillation of beams
		Approximate methods for determining natural frequencies
Chapter-11---Materials_2022_Aircraft-Structures-for-Engineering-Students
	Materials
		Steel
		Titanium
		Polymers
		Glass
		Ceramics
		Composite materials
		Properties of materials
			Outline placeholder
				Ductility
				Brittleness
				Elastic materials
				Plasticity
				Isotropic materials
				Anisotropic materials
				Orthotropic materials
			Testing of engineering materials
				Tensile tests
				Compression tests
				Bending tests
				Shear tests
				Hardness tests
				Impact tests
			Stress-strain curves
				Low carbon steel (mild steel)
				Aluminum
				Brittle materials
				Composites
			Strain hardening
			Creep and relaxation
			Fatigue
Chapter-12---Structural-components-of-air_2022_Aircraft-Structures-for-Engin
	Structural components of aircraft and spacecraft
		Structural components: Aircraft
			Loads on structural components
			Function of structural components
			Fabrication of structural components
		Structural components: Spacecraft
			Outline placeholder
				Thrust structure
				Stage structures
				Adaptors
				Payload fairings
			Loads on structural components
		Connections
			Riveted connections
				Simple lap joint
				Rivet shear
				Bearing pressure
				Plate failure in tension
				Shear failure in a plate
			Joint efficiency
			Group-riveted joints
			Eccentrically loaded riveted joints
			Welded connections
			Use of adhesives
		References
Chapter-13---Airworthiness_2022_Aircraft-Structures-for-Engineering-Students
	Airworthiness
		Factors of safety: flight envelope
		Load factor determination
			Limit load
			Uncertainties in design and structural deterioration
			Variation in structural strength
			Fatigue
		Airworthiness: Spacecraft
			Factors of safety
		Reference
Chapter-14---Airframe-loads_2022_Aircraft-Structures-for-Engineering-Student
	Airframe loads
		Aircraft inertia loads
		Symmetric maneuver loads
			Level flight
			General case of a symmetric maneuver
		Normal accelerations associated with various types of maneuver
			Steady pullout
			Correctly banked turn
		Gust loads
			Sharp-edged gust
			The graded gust
			Gust envelope
		Design loads: Spacecraft
		References
Chapter-15---Fatigue_2022_Aircraft-Structures-for-Engineering-Students
	Fatigue
		Safe life and fail-safe structures
		Designing against fatigue
		Fatigue strength of components
		Prediction of aircraft fatigue life
		Crack propagation
			Stress concentration factor
			Crack tip plasticity
			Crack propagation rates
		References
		Further reading
Chapter-16---Bending-of-open-and-closed-_2022_Aircraft-Structures-for-Engine
	Bending of open and closed thin-walled beams
		Symmetrical bending
			Assumptions
			Direct stress distribution
			Anticlastic bending
		Unsymmetrical bending
			Sign conventions and notation
			Resolution of bending moments
			Direct stress distribution due to bending
			Position of the neutral axis
			Load intensity, shear force, and bending moment relationships, the general case
		Deflections due to bending
			Singularity functions
			Moment-area method for symmetrical bending
		Calculation of section properties
			Parallel axes theorem
			Theorem of perpendicular axes
			Second moments of area of standard sections
			Product second moment of area
			Approximations for thin-walled sections
		Applicability of bending theory
		Temperature effects
		Reference
Chapter-17---Shear-of-beams_2022_Aircraft-Structures-for-Engineering-Student
	Shear of beams
		General stress, strain, and displacement relationships for open and single-cell closed section thin-walled beams
		Shear of open section beams
			Shear center
		Shear of closed section beams
			Twist and warping of shear-loaded closed section beams
			Shear center
		Reference
Chapter-18---Torsion-of-beam_2022_Aircraft-Structures-for-Engineering-Studen
	Torsion of beams
		Torsion of closed section beams
			Displacements associated with the Bredt-Batho shear flow
			Condition for zero warping at a section
		Torsion of open section beams
			Warping of the cross-section
Chapter-19---Combined-open-and-closed-_2022_Aircraft-Structures-for-Engineer
	Combined open and closed section beams
		Bending
		Shear
		Torsion
Chapter-20---Structural-idealiza_2022_Aircraft-Structures-for-Engineering-St
	Structural idealization
		Principle
		Idealization of a panel
			Unsymmetrical sections
		Effect of idealization on the analysis of open and closed section beams
			Bending of open and closed section beams
			Shear of open section beams
			Shear loading of closed section beams
			Alternative method for the calculation of shear flow distribution
			Torsion of open and closed section beams
		Deflection of open and closed section beams
Chapter-21---Wing-spars-and-box-_2022_Aircraft-Structures-for-Engineering-St
	Wing spars and box beams
		Open and closed section beams
		Beams having variable stringer areas
Chapter-22---Fuselages_2022_Aircraft-Structures-for-Engineering-Students
	Fuselages
		Bending
		Shear
		Torsion
		Pressurized fuselages
		Cut-outs in fuselages
		Reference
Chapter-23---Wings_2022_Aircraft-Structures-for-Engineering-Students
	Wings
		Three-boom shell
		Bending
		Torsion
		Shear
		Shear center
		Tapered wings
		Deflections
		Cut-outs in wings
Chapter-24---Fuselage-frames-and-wi_2022_Aircraft-Structures-for-Engineering
	Fuselage frames and wing ribs
		Principles of stiffener/web construction
		Fuselage frames
		Wing ribs
Chapter-25---Spacecraft_2022_Aircraft-Structures-for-Engineering-Students
	Spacecraft
		Natural frequencies
		Axial stress
		Stability
		Reference
Chapter-26---Laminated-composite-st_2022_Aircraft-Structures-for-Engineering
	Laminated composite structures
		Elastic constants of a simple lamina
		Stress-strain relationships for an orthotropic ply (macro approach)
			Specially orthotropic ply
			Generally orthotropic ply
		Laminates
			Assumptions and notation
			Laminate under in-plane loading
			Equivalent elastic constants
			Laminate strengths
		Thin-walled composite beams
			Axial load
			Bending
			Shear
				Open section beams
				Closed section beams
			Torsion
				Closed section beams
				Open section beams
			Idealization of composite beams
		References
Chapter-27---Closed-section-be_2022_Aircraft-Structures-for-Engineering-Stud
	Closed section beams
		General aspects
		Shear stress distribution at a built-in end of a closed section beam
		Thin-walled rectangular section beam subjected to torsion
		Shear lag
		Reference
Chapter-28---Open-section-bea_2022_Aircraft-Structures-for-Engineering-Stude
	Open section beams
		I-Section beam subjected to torsion
		Torsion of an arbitrary section beam
		Distributed torque loading
		Extension of the theory to allow for general systems of loading
		Moment couple (bimoment)
			Shear flow due to MΓ
		References
Chapter-29---Wing-problems_2022_Aircraft-Structures-for-Engineering-Students
	Wing problems
		Load distribution and divergence
			Wing torsional divergence (two-dimensional case)
			Wing torsional divergence (finite wing)
			Swept wing divergence
		Control effectiveness and reversal
			Aileron effectiveness and reversal (two-dimensional case)
			Aileron effectiveness and reversal (finite wing)
		Introduction to ``flutter´´
			Coupling
			Determination of critical flutter speed
			Prevention of flutter
			Experimental determination of flutter speed
			Control surface flutter
		References
Appendix---Design-of-a-rear-fuse_2022_Aircraft-Structures-for-Engineering-St
	Appendix: Design of a rear fuselage
		Specification
		Data
		Aircraft
		Wing
		Tailplane
		Fin
		Initial calculations
			Flight envelope
			Fin lift-curve slope
			Speed of sound
		Balancing out calculations
			Case A
		Fuselage loads
			Fuselage section
			Material
			Self-weight
			Shear forces and bending moments due to self-weight
			Total shear forces bending moments and torques
		Fuselage design calculations
			Stringer sections
				Skin thickness
				Rivet size
					Skin/stringer rivets
					Frame/stringer rivets
Index_2022_Aircraft-Structures-for-Engineering-Students
	Index
		A
		B
		C
		D
		E
		F
		G
		H
		I
		L
		M
		N
		O
		P
		Q
		R
		S
		T
		U
		V
		W
		Y
		Z