ES196 Engineering Structures Flashcards

1
Q

Reaction forces

A

Develop when an external force is applied to a body

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2
Q

If two forces have intersecting lines of action

A

They combine as vectors and act at the point of intersection

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3
Q

Principle of transmissibility

A

If a force is translated along its line of action - size of moment of force doesn’t change

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4
Q

Convenience of line of action

A

In practice, force acts at a point, but line of action allows force to be translated without affecting moment

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5
Q

Moment of a couple

A

Force x distance between points of application of force

(independent of reference point)

(r2-r1)xP

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6
Q

What causes an internal force

A

An external force haha!

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7
Q

Types of loads on a beam

A

Concentrated load (at a point)
Distributed load N/m
Reaction forces (forces holding beam up)

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8
Q

The moment of a force

A

describes the tendency of a rigid
body to rotate and is characterised by a force, a centre of
rotation and the perpendicular distance between centre of
rotation and point of application of the force

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9
Q

Static and Kinetic friction

A

Static friction is the friction present between two or more objects that are not moving with respect to each other. Kinetic friction is the friction present between two or more objects that are in motion with respect to each other.

Fs ≤ μsN
Fd = μkN
Usually μk is less than μs

https://www.youtube.com/watch?v=RIBeeW1DSZg last q

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10
Q

Fluid definition

A

A fluid is any continuous
substance which, when at
rest, exerts only normal
forces on its boundary
surfaces
Fluids may be either
liquids (hydrostatic
pressure) or gases (aerostatic pressure)

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11
Q

Types of loads

A

Dead - self weight
Live - people, cars, moveable furniture (assumed by designer)
Environmental - Loads that act due to weather/natural stuff

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12
Q

Types of support

A

Roller support - 1 unknown, orthogonal to surface its on (allows movement parallel to surface + rotation)
Pin joint - 2 unknowns, x and y components
(allow for rotation, no translation)
Fixed support - x,y and reaction moment
(no translations/rotations)

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13
Q

If a certain degree of freedom is restrained at a support

A

There will be a corresponding reaction force/moment

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14
Q

Why trusses are more efficient than beams (qualitative)

A

All material is being used close to failure stress, however beams act in bending and a lot of material is not under stress

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15
Q

Compression vs tension members

A

Compressive members break easier esp when long

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16
Q

Conditions for a truss system to not collapse

A

All connections between members must be “pins”, that is connections that allow members to
rotate relative to each other. If this is not the case, bending may occur in members
* All loads on a truss must be applied at the “nodes” where members meet. Again, if this is not
the case members will be in bending and inefficiently used.
* Trusses must consist of a number of triangles

In triangles, you cannot change the angle between pins (deflection) without changing the length of a side.

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17
Q

Deriving performance index

A
  • Don’t want objective to depend on design properties (free variables), only materials
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18
Q
A
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19
Q

Relationship between sf and bm diagrams

A

dv/dx = -w where w is distributed load
So change in v = area under loading diagram

DM/dx = V

Change in M = area under sf diagram

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20
Q

Warren truss

A

Symmetrical

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21
Q

Bending moment at a pin joint

A

Zero bending moment - as rotation isn’t restricted, so there will be no moment reaction

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22
Q

Zero force members

A

3 members connected at a joint, with two aligned. Only one member has component in vertical direction, so vertical must carry no force.

Other when two members at a joint, and aren’t aligned, both must be zero force

True when no external load on members
Can remove zero force members from example

Used to prevent buckling of longer members, and unexpected loads won’t cause structures to fail

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23
Q

Condition for principle of superposition of forces for beams

A

Linear system (in linear elastic range)

WITHIN ELASTIC LIMIT

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24
Q

Lever rule

A

a1F1 = a2F2

Where a is respective distance to force on beam

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25
Q

Equilibrium conditions for body in 3d

A

6

26
Q

Quick way to check statically indeterminacy

A

If a reaction can be removed without allowing any rigid body motion/mechanisms

27
Q

Number of bars and joints in statically determinante planar truss

A

B=2j-3

28
Q

Why there is no bm at pin and roller joints

A

Rotation is permitted

29
Q

3 point bending

A

Simply supported beam w vertical force in middle

30
Q

Characteristic strength

A

Maximum structural capacity

31
Q

Types of stress

A

Direct stress σ (axial force and bending moment)
Perpendicular to cross section
Shortening/elongation

Shear stress τ (shear force and torsion)
Parallel to cross section
Distortion

32
Q

Longitudinal line for beam

A

Neutral plane - remains at original length, no tension/compression

In positive bending, compression on top, tension under. Direct stress varies linearly above/below line

Neutral axis goes through com

33
Q

Elastic theory

A

Objects deforms when a pair of forces are applied, if material is elastic it’ll return to its original shape when the forces are removed

Perfect elasticity is an approximation
Few materials remain purely elastic even after small deformations

34
Q

Shear modulus/modulus of rigidity (G)

A

Object tendency to shear (deformation at constant volume) defined as shear stress/shear strain

35
Q

Homogeneous and isotropic materials

A

Homogeneous - composition is uniform throughout

Isotropic - how material responds when certain force is applied (response changing depending on direction of load)

Homogeneous and isotropic - steel
Wood - heterogeneous and anisotropic
Concrete - heterogenous, isotropic

36
Q

Nominal/engineering stress and strain

A

Stress is force over original area
Not true stress as area changes
Stress delta over og
Not true strain as “og” is changing

37
Q

Nominal/engineering stress and strain

A

Stress is force over original area
Not true stress as area changes
Stress delta over og
Not true strain as “og” is changing

38
Q

Stress and strain

A

In same direction

39
Q

Modulus of rigidity

A

E/2(1+v) poissons ratio (measure of lateral deformation)

40
Q

Yielding, strain hardening, necking

A
  • sudden change in length at constant stress
  • disproportionality
  • cross section decreases then breaks
41
Q

Ductility

A

Material that can be subjected to large strains before fracture

Percent elongation Lf-L0/L0 . 100
Perfect reduction in area A0-… U get

42
Q

Brittle

A

Material that exhibits little/no yielding before failure

43
Q

Isotropic Vs anisotropic materials

A

Showing physical behaviour (deformation) that doesn’t change depending on direction of load

44
Q

Longitudinal Vs lateral strains

A

Longitudinal in the same direction as the load, lateral perpendicular

45
Q

Poissons ratio

A

Negative ratio of lateral/longitudinal strain

Within elastic range of material this is constant
Unique for a homogeneous and isotropic material

Materials used in engineering practice 0≤v≤0.5

46
Q

Assumptions in beams

A

Material is linear elastic homogenous and isotropic
Cross sections which are plane and normal to longitudinal axis remain so after deformation
Beam deflections are small
Beam is long and slender
length»width n depth

47
Q

Structural rigidity

A

Resistance offered by a beam while undergoing deformation (EI)

48
Q

Neutral plane

A

Goes through longitudinal axis

49
Q

Moment of inertia/second moment of area

A

Measures an objects resistance to bending
(about a given axis) neutral axis in subscript

Rectangular cross section bh^3/12
b is in same direction of neutral axis
units length^4

50
Q

Qualitative deduction of higher moi

A

Greater material further from bending axis - better at resisting bending motion - higher moi

Area moi reflects how area of a cross section is distributed relative to an axis

always positive due to square

can be added and subtracted e.g. rectangle w circular hole take I for rectangle minus I for hole

51
Q

Kernel of a cross section

A

The area, within which a normal compressive
force will not produce tension in the cross-section, is called the kernel of the
cross-section

52
Q

Relation between longitudinal axis and vertical plane along beam

Also any deformation of cross section in own plane due to bending moment is neglected

A

Always 90⁰

53
Q

Why must a beam be adequately supported

A

To permit transfer of loads to supports

54
Q

Neglections in bernouilli beam theory

A

Shear deformations
assumption that the shear
force Q(x) does not contribute directly to the deformation of the beam
deflections small and elastic
applies to slim beams (l/d>20)

55
Q

Beam support conditons

(bernuly eq)

A

Free - M=0 V=0
simple supports M=0 Y=0
Fixed Y=0 θ=0

The beam must be supported by at least the number of constraints that
prevent free motion. However, many structures have more supports than
strictly needed to fix the structure in the plane or in space. Extra supports and
extra connections between structural elements typically increase the stiffness
of the structure, while rendering the structure statically indeterminate.

56
Q

Relating rotation and vertical deflection

A

θ=-dy/dx

57
Q
A
58
Q

What allows for cross section to remain tangent to elastic line at a point

A

Shear stresses I think

59
Q

What allows for cross section to remain tangent to elastic line at a point

A

Shear stresses I think

60
Q

Values of shear in beam bending (wooden block model)

A

0 at top and bottom, non zero in middle

61
Q

Failure in torsion ductile Vs brittle

A

Ductile tends to fail perpendicular to longitudinal axis, as they tend to fail in shear, so fracture along plane of maximum shear stress.

Brittle materials fail along 45 degrees. Brittle materials tend to fail along maximum tensile stress. Weaker in tension than in shear