Mechanical Systems V - Statics Flashcards



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  • Force and Moment: 3D Reminders

Rectangular Components (3D)

A force vector F\mathbf{F} can be expressed in terms of its rectangular components:

  • Vector form: F=Fx+Fy+Fz\mathbf{F} = \mathbf{F}_x + \mathbf{F}_y + \mathbf{F}_z

  • Unit vector notation: F=Fxi+Fyj+Fzk\mathbf{F} = F_x \mathbf{i} + F_y \mathbf{j} + F_z \mathbf{k}

Determination of the projection of F\mathbf{F} on each axis using direction cosines:

  • Fx=Fcos⁡(θx)F_x = F \cos(\theta_x)

  • Fy=Fcos⁡(θy)F_y = F \cos(\theta_y)

  • Fz=Fcos⁡(θz)F_z = F \cos(\theta_z)

Magnitude calculation:

  • F=Fx2+Fy2+Fz2F = \sqrt{F_x^2 + F_y^2 + F_z^2}

Moment (3D)

While scalar multiplication (moment-arm rule) is convenient for 2D, 3D analysis requires a vector approach involving cross-product multiplication because determining perpendicular distances between lines of action and points is computationally tedious.

Evaluation of the cross product at point OO:

  • M0=OA×F=(rxryrz)×(FxFyFz)=(MxMyMz)\mathbf{M}_0 = \mathbf{OA} \times \mathbf{F} = \begin{pmatrix} r_x \\ r_y \\ r_z \end{pmatrix} \times \begin{pmatrix} F_x \\ F_y \\ F_z \end{pmatrix} = \begin{pmatrix} M_x \\ M_y \\ M_z \end{pmatrix}

  • Expansion of components:

    • Mx=ryFz−rzFyM_x = r_y F_z - r_z F_y

    • My=rzFx−rxFzM_y = r_z F_x - r_x F_z

    • Mz=rxFy−ryFxM_z = r_x F_y - r_y F_x

Couple (3D)

A couple magnitude is calculated as follows:

  • M=rA×F+rB×(−F)=(rA−rB)×F\mathbf{M} = \mathbf{r}_A \times \mathbf{F} + \mathbf{r}_B \times (-\mathbf{F}) = (\mathbf{r}_A - \mathbf{r}_B) \times \mathbf{F}

  • Letting r=rA−rB\mathbf{r} = \mathbf{r}_A - \mathbf{r}_B, the formula simplified becomes: M=r×F\mathbf{M} = \mathbf{r} \times \mathbf{F}

  • Key Properties of Couples:

    • The couple is identical about all points; reference to the moment center OO disappears.

    • A couple is a free vector in 3D.

    • In contrast, the moment of a force about a point is a sliding vector directed along the axis through that point.

Resultants (3D)
  • Force Resultant: The simplest force combination that can replace original forces without changing the external effect on a rigid body. Equilibrium occurs when the resultant of all forces acting on a body is zero.

    • R=∑F=F1+F2+F3+…\mathbf{R} = \sum \mathbf{F} = \mathbf{F}_1 + \mathbf{F}_2 + \mathbf{F}_3 + \dots

  • Principle of Moments: The moment resultant is the sum of all individual moments at a specific point (e.g., point OO).

    • M0=∑(ri×Fi)=M1+M2+M3+…\mathbf{M}_0 = \sum (\mathbf{r}_i \times \mathbf{F}_i) = \mathbf{M}_1 + \mathbf{M}_2 + \mathbf{M}_3 + \dots

Representation of Distributed Loads

Forces can be distributed across a surface or length in three common ways:

  1. Uniformly distributed load: Represented as a constant rectangular profile.

  2. Uniformly varying load: Represented as a triangular profile.

  3. Uniformly distributed and varying load: A trapezoidal combination of constant and varying profiles.

Mechanical Actions

Link Diagrams and System Isolation
  • Physical System: A set of materials with constant mass over time.

  • System Boundary: To study a solid in statics, it must be isolated via an imaginary border separating the internal part (Σ\Sigma) from the external part (Σˉ\bar{\Sigma}).

  • Mechanical Action Diagram: Visualizes external actions. Example with solids 00, 11, and 22:

    • If isolating solid 11: The balance includes external actions on 11 (ext →1\rightarrow 1), connection action from 22 (2→12 \rightarrow 1), and connection action from 00 (0→10 \rightarrow 1).

    • If isolating system A={1+2}A = \{1 + 2\}: The balance includes ext →1\rightarrow 1, ext →2\rightarrow 2, 0→10 \rightarrow 1, and 0→20 \rightarrow 2. Note that 2→12 \rightarrow 1 becomes an internal mechanical action and is excluded from the balance.

Mechanical Action Torsor

A mechanical action of solid S1S1 on S2S2 is defined by two vectors reducing to a specific point (reduction point):

  1. Resultant (Pushing action): R\mathbf{R}.

  2. Moment (Twisting action): MO\mathbf{M}_O.

Representation of the Torsor:

  • {τS1→S2}={X12L12Y12M12Z12N12(O,x,y,z)\{\tau_{S1 \rightarrow S2}\} = \begin{cases} X_{12} & L_{12} \\ Y_{12} & M_{12} \\ Z_{12} & N_{12} \end{cases}_{(O, \mathbf{x}, \mathbf{y}, \mathbf{z})}

Summary of Kinematic Joints

Each joint is defined by its degrees of freedom (ncn_c) and degrees of connection (nsn_s). Below are the details for various joints:

  • Fixed Joint (nc=0n_c = 0, ns=6n_s = 6):

    • Kinematic Torsor: All elements are zero.

    • Action Torsor: {X12L12Y12M12Z12N12\begin{cases} X_{12} & L_{12} \\ Y_{12} & M_{12} \\ Z_{12} & N_{12} \end{cases}.


Power and Perfect Joints

Developed Power

The power developed by an action jj on solid SS at time tt in reference frame (R)(R) using torsor τ\tau at point MM:

  • PR({τS/j})={τS/j}⋅{VS/R}P_{R}(\{\tau_{S/j}\}) = \{\tau_{S/j}\} \cdot \{\mathcal{V}_{S/R}\}

  • Expanded form: PR({τS/j})=R({τS/j}M)⋅v({VS/R}M)+M({τS/j}M)⋅ω({VS/R}M)P_{R}(\{\tau_{S/j}\}) = \mathbf{R}(\{\tau_{S/j}\}_M) \cdot \mathbf{v}(\{\mathcal{V}_{S/R}\}_M) + \mathbf{M}(\{\tau_{S/j}\}_M) \cdot \mathbf{\omega}(\{\mathcal{V}_{S/R}\}_M)

Perfect Kinematic Joint

A joint is considered perfect if there is no gap and no friction. In this case, the power developed between the two solids is zero:

  • P({τS2/S1})={τS2/S1}⋅{VS1/S2}=0P(\{\tau_{S2/S1}\}) = \{\tau_{S2/S1}\} \cdot \{\mathcal{V}_{S1/S2}\} = 0

  • Example (Hinge of axis x\mathbf{x}): The rotation exists only around xx, but the action torsor has a zero moment component L12L_{12} along xx, resulting in zero power.

Fundamental Principle of Statics (FPS)

Theoretical Theorems
  • General Theorem: If a physical system is in static equilibrium, the total external mechanical action torsor applied on Σ\Sigma is null:

    • {τΣ→Σˉ}={0}\{\tau_{\Sigma \rightarrow \bar{\Sigma}}\} = \{0\}

  • Theorem of Static Resultant: In equilibrium, the resultant of the external mechanical action torsor is zero:

    • R({τΣ→Σˉ})=0\mathbf{R}(\{\tau_{\Sigma \rightarrow \bar{\Sigma}}\}) = \mathbf{0}

  • Theorem of Static Moment: In equilibrium, the moment of the external mechanical action torsor calculated at any point AA is zero:

    • MA({τΣ→Σˉ})=0\mathbf{M}_A(\{\tau_{\Sigma \rightarrow \bar{\Sigma}}\}) = \mathbf{0}

  • Theorem of Reciprocal Actions: (Newton's Third Law) For systems in equilibrium, the torsor of Σ1\Sigma_1 on Σ2\Sigma_2 is the negative of the torsor of Σ2\Sigma_2 on Σ1\Sigma_1:

    • {τΣ2→Σ1}=−{τΣ1→Σ2}\{\tau_{\Sigma_2 \rightarrow \Sigma_1}\} = -\{\tau_{\Sigma_1 \rightarrow \Sigma_2}\}

Problem Solving Approach
  1. Step 1: Draw the link diagram.

  2. Step 2: Isolate the specific solid(s) for study.

  3. Step 3: Determine all mechanical action torsors acting on the isolated system(s).

  4. Step 4: Solve for unknowns by applying the FPS.

Beams

Determinacy and Stability
  • Determinate Structure: Unknown external reactions or internal members can be found using only equilibrium conditions.

  • Indeterminate Structure: Unknowns cannot be determined by statics alone; compatibility conditions of structural parts are required.

  • Mathematical Conditions:

    • Let RR = number of support reactions.

    • Let FiFi = number of reaction forces from internal hinges.

    • Let mm = number of members.

    • Statically Unstable: R+Fi<3mR + Fi < 3m

    • Statically Determinate and Stable: R+Fi=3mR + Fi = 3m

    • Statically Indeterminate: R+Fi>3mR + Fi > 3m

Free-Body Diagram (FBD)

The FBD is a simple visual representation of the mechanical action torsor components applied to the beam.

  • Example Components: Reactions at supports (e.g., Ax,Ay,MAA_x, A_y, M_A at point AA, ByB_y at point BB), beam length LL, and external point loads PP.

Beam Problem Solving Approach
  1. Step 1: Draw the FBD, replacing distributed loads with simplified representations and identifying all torsor components.

  2. Step 2: Check stability and determinacy. If the structure is unstable or indeterminate, isolate multiple specific beams to solve.

  3. Step 3: Solve for components of the mechanical action torsor using FPS (decomposing into resultants and moments).