Statics Flashcards

1
Q

What is the layout of a 2D rotation matrix?

A

[cosϕ, sinϕ]
[-sinϕ, cosϕ]

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2
Q

How do you convert a vector between the original and rotated coordinate systems?

A

[v’] = [R][v]
[v] = [R]T[v’]

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3
Q

How do you convert a matrix between the original and rotated coordinate systems?

A

[A’] = [R][A][R]T
[A] = [R]T[A’][R]

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4
Q

What does the ‘prime’ indicator show of a vector or matrix?

A

Aligned with the bar axis

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5
Q

What is the Euler-Bernoulli displacement matrix equation?

A

[x’] = [x+u(x)] + y[-sin𝛙(x)]
[y’] [ w(x) ] [ cos𝛙(x)]

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6
Q

What is assumed by the Euler-Bernoulli model?

A

Zero shear
Planes are consistent
Planes remain orthogonal to the neutral axis

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7
Q

What is the Neutral Axis displacement angle according to the small angle assumption?

A

𝛙 = dw/dx

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8
Q

What is εyy for Euler-Bernoulli bars?

A

εyy = 0

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9
Q

What is εxx for Euler-Bernoulli bars?

A

εxx = -y(d2w/dx2)

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10
Q

What does the curvature χ symbolise?

A

χ = d2w/dx2

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10
Q

What is the simplified equation for the z moment?

A

Mz = EIχ

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11
Q

What is the function, f, for the Euler-Bernoulli strong form?

A

f = EI(d4w/dx4)

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12
Q

How is shear force Q derived from the moment?

A

Q = dM/dx

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13
Q

Which essential boundary conditions cannot coexist at the same point?

A

ΓQ & Γw or ΓM & Γθ

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14
Q

What must be true for the Euler-Bernoulli weak form to work?

A

Test function δw must be C1 continuous

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15
Q

What does C1 continuity mean?

A

The function and its first derivative are both continuous

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16
Q

How is a physical domain (x1 - x2) translated to a parent domain (-1 < ξ < 1)

A

ξ = (2(x-x1)/le) - 1

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17
Q

Why is a parent domain used?

A

Shape functions for a parent domain are easier to find

18
Q

What is the gradient of the w shape functions at the extents?

A

Gradient of zero at -1 and 1

19
Q

What are the gradients of the θ shape functions at the extents?

A

For Nθ1, the gradient is 1 at -1 and 0 at 1
For Nθ2, it is 0 at -1 and 1 at 1

20
Q

How do the shear and moment matrices affect the deflections?

A

Q (shear) matrix affects w (vertical deflection), M (moment) matrix affects θ (angular deflection)

21
Q

How are the matrix properties of a frame created?

A

A combination of bar and beam properties, where bar parts constitute ux and beam parts contribute uy and θ

22
Q

What are γ and β in Timoshenko Beam Theory?

A

γ is shear angle
β is rotation of fibre

23
Q

What is the curvature χ for Timoshenko Theory?

A

dβ/dx

24
Q

What is warping?

A

When plane sections do not remain planar

25
Q

What is shear force Q in Timoshenko Theory?

A

Q = GAγ

26
Q

How are slender and stocky beams defined?

A

L/t >= 20, Slender
L/t < 10, Stocky

27
Q

For what kind of beams do Timoshenko and Euler-Bernoulli diverge significantly?

A

Stocky beams

28
Q

Why is the correction factor κ introduced for Timoshenko?

A

Because γ is overcorrected by the method

29
Q

What is the value of κ for rectangular beams?

A

κ = 5/6

30
Q

What is the benefit of using beam theory over 3D elastic theory

A

The reduced beam theory is far simpler than the full theory and allows for efficient numerical implementation.

31
Q

How do you begin the derivation of the horizontal translation u(x,y)?

A

u(x,y) = -y sinθ

32
Q

How do you find the shear strain εxy?

A

2εxy = du/dy + dw/dx

33
Q

How do you find the moment on an area A, caused by stress σ at distance y?

A

M = -∫ yσ dA

34
Q

Simplify the balance of forces equation Q(x + Δx) - Q(x) + f(x + Δx/2)Δx = 0

A

dQ + fdx = 0
Therefore dQ/dx = -f

35
Q

Why is C1 continuity important?

A

f and δf and their derivatives have to be continuous for the integral in the weak form to work

36
Q

How are the element stiffness matrix Ke and the shape factor vector Be related?

A

Ke = ∫ Ee Ie BeT Be dx

37
Q

What is the vector Be?

A

The vector of second derivatives of the shape functions Ne

38
Q

For Euler-Bernoulli theory, what are the shape functions Ne functions of?

A

Ne(w) are functions of ξ
Ne(θ) are functions of ξ and Le

39
Q

What are the 3 steps for finding the Euler-Bernoulli weak form?

A
  • Multiply (S) with an arbitrary test function δw.
  • Integrate the result over the length of the bar.
  • Perform an integration by parts twice.
40
Q

What is assumed by Timoshenko Theory?

A

A plane section normal to the centroid remains plane but undergoes shear deformation

41
Q

What is the required continuity for w and β in the Timoshenko weak form?

A

C0 continuity

42
Q

What is dw/dx - β representative of in the Timoshenko weak form?

A

γ