Stability & Determinance

Three Important Relationships

The following three relationships are used to solve different types of structural mechanics problems.

Relationship Description
Equilibrium
つり合い
Relationship between forces and stresses
Based on Newton's laws of motion: the sum of all forces acting on a structure at rest is zero.
Constitutive Relationships
構成則
Relationship between stress and strain
Based on the element's material properties and how it reacts to forces. A key example is Hooke's law, which describes linear-elastic material behavior.
Compatibility
適合
Relationship between strain and displacement
Describes geometry of deformation such that there is no rupture or overlapping of the material.

Force → (Equilibrium) → Stress → (Constitutive) → Strain → (Continuity) → Displacement

On the First Class Architect exam, you will need to be able to use the equations of equilibrium. You will also need to understand how to leverage compatibility and constitutive relationships, although you won't necessarily need to use formal equations, etc.

Constitutive Relationships

As mentioned above, the typical example of a constitutive relationship is Hooke's law: \(F=kx\). This is used to describe spring stiffness and is commonly used, e.g. axial stiffness: \(k=\frac{AE}{L}\). Another form of this same law is well known to engineers and describes the elastic stress-strain relationships: \(\sigma=E\epsilon\) or \(\gamma=G\tau\).

Continuity

You don't need to set up continuum equations, but you do need to identify basic contintuity conditions, i.e., displacement or slope continuity. Example:

Positive Convention

It's important to use a consistent convention for positive forces and moments. The tricky part is that these mean different things, depending on whether you're looking at externally applied forces or internal stresses.

External Forces

For external forces, typically forces acting upwards and rightwards are positive. The US uses the right-hand-rule (RHR), which dictates that positive moments spin counter-clockwise (CCW). In Japan, it's common to defined positive applied moments as spinning clockwise (CW), which is the opposite of the RHR.

Internal Forces

Both countries use the same convention for internal forces:

Equilibrium

Structures in equilibrium satisfy the following three expressions, regardless of the point of reference.

Equations of Equilibrium
$$\sum F_X=0$$ $$\sum F_Y=0$$ $$\sum M=0$$

NOTE: Setting up the equations of equilibrium is a critical step in solving many structural analysis and free-body diagram problems.

Supports and Joints

External Supports

There are four main types of boundary conditions, illustrated in the table below. Typically, the reactions at supports are thought of in terms of a global frame of reference: Fx, Fy and M.

Boundary Conditions
Free Roller Pin Fixed
No reactions 1 reaction 2 reactions 3 reactions

Internal Joints

There are several types of internal joints, which are different releases (degrees of freedom) for forces and moments acting within the structure.

Types of Internal Joints
Rigid Pin Axial Slider Shear Slider
No releases Moment release Axial release Shear release

Stability of Structures

Types of Structures
Unstable
不安定
Stable
安定
Determinant
静定
Indeterminant
不静定
Unstable structures that do not satisfy equilibrium equations. Stable structures that can be solved with only equilibrium equations. Stable structures that require compatibility or constitutive equations in addition to equalibrium equations.

There are several methods for rapidly assessing whether a simple 2D structure is unstable, determinant or indeterminant.

Japanese Method

The following equation is the commonly used in Japan, although it generates the same results as the alternative below.

\(m<0\) (Unstable) $$m=n+s+r-2k$$
\(m=0\) (Determinant)
\(m>0\) (Indeterminant)

The defintion of each of these variables are as follows:

Example Frame

Example Frame

NOTE: the number of support reactions (n) is the sum of reactions at each individual support, based on the boudnary conditions. Refer to External Supports above.

Counting Nodes (k)

The illustration belows shows the example frame with all the nodes numbered. Nodes are the supports, joints and free-ends of members. Think of them as the dots you'd first have to draw, then connect with lines, to illustrate the structure.

Frame with Nodes Labeled

Counting Members Segments (s)

In this method, rather than counting physical members, you must count the number of segments between the nodes. This is why it's helpful to count the nodes first. For example, the three members a-b, c-d-e and f-g are single physical elements in reality, but count as seven segments in this example.

Frame with Members Labeled

Counting rigid connections (r)

The figure shows a joint with four members (s=4) framing into it. In this case, one of the members is pinned at the joint, the others are rigidly connected. In this case r = 2 because the the maximum number of rigid joints at a node is the number of members framing into it minus 1. Another way to think of it: \(r_{joint}=s_{joint}-pins_{joint}-1\).

Four-way connection

The same four-way connection with no pins would have r = 3.

Example Conclusion

Totalling up each of these components gives us the value m:

$$m=n+s+r-2k=6+10+7-2(10)=3$$

Since m > 0, it's clear the structure is indeterminant. In this case it's indeterminant to the third degree, which means we'll need to use equations of compatibility and/or the constitutive relationships in addition to equilibrium to analyze this structure.

For the purposes of the First Class Architecture exam, you'll only need to rapidly assess whether a frame is unstable, determinant or indeterminant. The degree and force analysis are generally not required.

Alternative Method

In North America and Europe, the following method is used. It is very similar, but groups the equalibrium equations slightly differently.

\(d<0\) (Unstable) $$d=3m+r-3j-c$$
\(d=0\) (Determinant)
\(d>0\) (Indeterminant)

The defintion of each of these variables are as follows:

In this case the coefficient of 3 on members and joints comes from the fact that equalibrium satisifies three equations for each member and joint.

Which ever method is easier to remember is completely fine. They both yield the same results everytime.

Example Conclusion

Extending the example from above and summing for d:

$$d=3m+r-3j-c=3(10)+6-3(10)-3=3$$

This demonstrates that the two approaches yeild the same results.

NOTE: Several quantities in both methods are the same, but with different coefficient letters: m (US) = s (Japan), r (US) = n (Japan), j (US) = k (Japan). The key difference is the US method totals internal hinge quantity (c), while the Japanese approach totals the internal rigid joints (r).