basic structural theory

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Basic structural theory

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Basic structural theory. Statics Things don’t continue to move if forces are resisted – Static Equilibrium What resists the force? Equal and opposite Reaction Things deflect if forces are resisted Elastic and Plastic Deformation. Basic loads (forces) Vertical (y only) Lateral (x only) - PowerPoint PPT Presentation

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Page 1: Basic structural theory

Basic structural theory

Page 2: Basic structural theory

Statics

Things don’t continue to move if forces are resisted – Static

Equilibrium

What resists the force? Equal and opposite Reaction

Things deflect if forces are resisted

Elastic and Plastic Deformation

Page 3: Basic structural theory

Basic loads (forces)

Vertical (y only)

Lateral (x only)

Rotational (moment)

Concentrated loads

Distributed loadsw = P/l

force-couple

Page 4: Basic structural theory

Basic components

Linear – Column, Beam

Planar – Wall, Floor

Page 5: Basic structural theory

Basic connections

Simple (constrain y in direction of gravity, rotate freely)

Page 6: Basic structural theory

Basic connections

Roller (constrain y, rotate freely)

Page 7: Basic structural theory

Basic connections

Pin (constrain x & y, rotate freely)

Page 8: Basic structural theory

Basic connections

Pin (constrain x & y, rotate freely)

Page 9: Basic structural theory

Basic connections

Cable (Pin with tension only)

Page 10: Basic structural theory

Basic connections

Cable (Pin with tension only)

Page 11: Basic structural theory

Basic connections

Fixed/Rigid (constrain x, y, rotation)

Page 12: Basic structural theory

Basic connections

Fixed/Rigid (constrain x, y, rotation)

Page 13: Basic structural theory

Basic connections

Fixed/Rigid (constrain x, y, rotation)

Page 14: Basic structural theory

Basic connections

Fixed/Rigid (constrain x, y, rotation)

Page 15: Basic structural theory

Basic connections

Misleading pin connections

Page 16: Basic structural theory

Column – Vertical Load

Axial load – Compression & Tension

Page 17: Basic structural theory

Column – Lateral Load

Non-axial (lateral) load – Buckling in compression

Page 18: Basic structural theory

Beam – Vertical Load

Non-axial load – Deflection

Page 19: Basic structural theory

Basic loads (forces)

Reactions are the same for Concentrated loads and Distributed

loads

Beam stresses are different

w = P/l

Page 20: Basic structural theory

Greater deflection

Greater max. moment

w = P/l

Page 21: Basic structural theory

CN

T

Beam – Stresses

Compression, Tension, Neutral axis

Page 22: Basic structural theory

Beam – Concentrated Vertical Load

Resist bending with Moment connection

Greater deflection

Greater max. moment

Page 23: Basic structural theory

Beam – Distributed Vertical Load

Resist bending with Moment connection

Greater deflection

Greater max. moment

Page 24: Basic structural theory

Factors influencing deflection:

P = load

l = length between supports

E = elastic modulus of material (elasticity)

I = Moment of inertia (depth/weight of beam)

Dmax = Pl 3/48EI

Page 25: Basic structural theory

Elastic modulus of materials

Structural Steel = 200 GPa (29,023,300 lb/in2)

Titanium = 110 GPa (15,962,850 lb/in2)

Aluminum = 70 GPa (10,158,177 lb/in2)

Concrete = 21 GPa (3,047,453 lb/in2)

Douglas Fir = 13 GPa (1,886,518 lb/in2)

Why are titanium and aluminum used in aircraft?

Page 26: Basic structural theory

Yield Strength of materials

Structural Steel=350-450 MPa

Titanium (Alloy)=900-1400 MPa

Aluminum=100-350 MPa

Concrete=70 MPa (compressive)

Douglas Fir= N/A

Density of materials

Structural Steel = 489 lb/ft3

Titanium = 282 lb/ft3

Aluminum = 169 lb/ft3

Concrete = 150 lb/ft3

Douglas Fir = 32 lb/ft3

1 lb/in2 = 6891 Pa

Page 27: Basic structural theory

Moment of Inertia of beam

Dependent on cross-sectional geometry

Not dependent on material properties

Icc = Moment of inertia of a rectangle about the neutral axis – i.e. it’s centroid = width x height3 /12

Ixx = Moment of inertia of a rectangle about an axis parallel to the neutral axis = Icc + width x height x (distance between axes)2

Centroid = S (Area x distance to bending axis)/(Total area)

Page 28: Basic structural theory
Page 29: Basic structural theory

Triangulated frame (Truss) – increase depth of beam

Triangulated – all members axially loaded (truss) – no moments

Page 30: Basic structural theory

Triangulated frame (Truss) – increase depth of beam

Triangulated – all members axially loaded (truss) – no moments

Page 31: Basic structural theory

Rigid Frame – Vertical load

Reduce deflection: Rigid connection

Columns resist force and deflect

Page 32: Basic structural theory

Rigid Frame – Vertical load

Thrust develops at base of columns and must be resisted

(beam / foundation / grade beam)

Page 33: Basic structural theory

Cantilever

Moment connection

Page 34: Basic structural theory

Cantilever

Moment connection

tension

compression

moment (force-couple)

Page 35: Basic structural theory

Cantilevered Beam – Vertical load

Greater deflection

Greater max. moment

Page 36: Basic structural theory

Simple Frame – Vertical load

Reduce deflection at mid-span: Cantilever

Lesser deflection

Lesser max. moment

Page 37: Basic structural theory

Cantilever

Deflection - Resist bending with counterweight

Page 38: Basic structural theory

Frame – Lateral load

Racking

Page 39: Basic structural theory

Frame – Lateral load

Racking

Page 40: Basic structural theory

Frame – Lateral load

Triangulated – all members axially loaded (truss) – no moment

connections

Page 41: Basic structural theory

Frame – Lateral load

Triangulated – all members axially loaded (truss) – no moment

connections

Page 42: Basic structural theory

Frame – Lateral load

Rigid (moment-resisting) frame

Page 43: Basic structural theory

Frame – Lateral load

Rigid (moment-resisting) frame

Page 44: Basic structural theory

Frame – Lateral load

Shear-resisting (force in plane)

Page 45: Basic structural theory

Frame – Lateral load

Pre-engineered shear panel

Page 46: Basic structural theory

Frame – Lateral load

Pre-engineered shear panel

Page 47: Basic structural theory

Frame – Lateral load

Shear-resisting (force in plane)

Non-structural partitions

Page 48: Basic structural theory

Frame – Lateral load

Shear-resisting (force in plane)

Masonry must be grouted and steel-reinforced

Page 49: Basic structural theory

Funicular structures

Tension (Cable)

Compression (Arch)

Page 50: Basic structural theory

Funicular structures

Tension (Cable)

Compression (Arch)

Page 51: Basic structural theory

Funicular structures

Tension (Cable)

Compression (Arch)

Page 52: Basic structural theory

Non-Funicular structures

Page 53: Basic structural theory

Materials - Wood

Tension & compression, no rigid connection

Page 54: Basic structural theory

Materials - Wood

Unpredictable failure mode (non-uniform material – organic)

Page 55: Basic structural theory

Materials - Reinforced Concrete

Wide range of possible forms

Page 56: Basic structural theory

Materials - Reinforced Concrete

Compression and some tension (steel), rigid connection through rebar

Page 57: Basic structural theory

Materials - Reinforced Concrete

Catastrophic failure mode

Page 58: Basic structural theory

Materials - Reinforced Concrete

Catastrophic failure mode

Page 59: Basic structural theory

Materials - Reinforced Concrete

Lab testing

Page 60: Basic structural theory

Materials - Steel

Tension & compression

Page 61: Basic structural theory

Materials - Steel

Rigid connection through welding

Page 62: Basic structural theory

Materials - Steel

Plastic failure mode