Engineering Mechanics: Statics, Equilibrium, and Beam Analysis

Fundamentals of Mechanics and Units

  • Newton's Laws of Motion:
    • First Law: A particle originally at rest, or moving in a straight line with constant velocity, remains in this state unless acted upon by an unbalanced force.
    • Second Law: A particle acted upon by an unbalanced force F\mathbf{F} experiences an acceleration a\mathbf{a} in the direction of the force with magnitude proportional to the force:     F=ma\mathbf{F} = m\mathbf{a}
    • Third Law: Mutual forces of action and reaction between two interacting particles are equal in magnitude, opposite in direction, and collinear.
  • International System of Units (SI):
    • Length: Metre (m\text{m}
    • Time: Second (s\text{s}
    • Mass: Kilogram (kg\text{kg}
    • Force: Newton (N=kg⋅ms2\text{N} = \frac{\text{kg}\cdot\text{m}}{\text{s}^2}
  • Standard Unit Prefixes:
    • Giga (G\text{G}): 10910^9
    • Mega (M\text{M}): 10610^6
    • Kilo (k\text{k}): 10310^3
    • Milli (m\text{m}): 10−310^{-3}
    • Micro (μ\mu): 10−610^{-6}
    • Nano (n\text{n}): 10−910^{-9}

Force Vectors and Component Resolution

  • Cartesian Vector Representation:
    • Uses orthogonal dimensionless unit vectors i\mathbf{i} and j\mathbf{j} along the xx and yy axes:     F=Fxi+Fyj\mathbf{F} = F_x\mathbf{i} + F_y\mathbf{j}
  • Resolution of Coplanar Forces:
    • Calculated via direction angle θ\theta:     Fx=Fcos⁡(θ)F_x = F\cos(\theta)Fy=Fsin⁡(θ)F_y = F\sin(\theta)
    • Calculated via slope ratios (a:b:ca:b:c):     Fx=F(ac)F_x = F\left(\frac{a}{c}\right)Fy=F(bc)F_y = F\left(\frac{b}{c}\right)
  • Resultant Force of Concurrent Coplanar Forces:
    • Component sums:     FRx=∑FxF_{Rx} = \sum F_xFRy=∑FyF_{Ry} = \sum F_y
    • Resultant magnitude:     FR=FRx2+FRy2F_R = \sqrt{F_{Rx}^2 + F_{Ry}^2}
    • Direction angle measured from the reference axis:     θ=tan⁡−1(∣FRy∣∣FRx∣)\theta = \tan^{-1}\left(\frac{|F_{Ry}|}{|F_{Rx}|}\right)

Particle Equilibrium and Free-Body Diagrams (FBD)

  • Equilibrium Conditions for a Particle:
    • Net resultant force acting on a stationary or uniformly moving particle is zero:     ∑Fx=0\sum F_x = 0∑Fy=0\sum F_y = 0
  • Free-Body Diagram (FBD) Requirements:
    • Isolate the system or point from its physical surroundings.
    • Identify all external forces: active loads, applied weights (W=mgW = mg), contact reactions (normal and friction forces), and cable tensions.
    • Set up a reference coordinate frame to resolve oblique vectors.
  • Linear Elastic Spring Force:
    • Governed by Hooke's Law:     F=ksF = ks
    • Parameter kk represents spring stiffness (N/m\text{N/m}) and s=l−l0s = l - l_0 represents elongation or deformation from unstretched length l0l_0.

Moments and Rotational Tendency

  • Scalar Moment Calculation:
    • Measures the rotational tendency of a force about a specific point or pivot OO:     MO=FdM_O = Fd
    • dd is the perpendicular moment arm between the point OO and the force's line of action.
  • Sign Convention and Direction:
    • Direction is perpendicular to the force-arm plane following the right-hand rule.
    • Standard 2D convention treats counterclockwise rotation as positive and clockwise rotation as negative.
  • Resultant Moment of a Coplanar Force System:
    • Algebraic sum of individual moments:     MRO=∑(Fd)M_{RO} = \sum (Fd)

Moment of a force about a point

Rigid Body Equilibrium and Support Reactions

  • Equilibrium Equations in Two Dimensions:
    • Completely prevents translation and rotation:     ∑Fx=0\sum F_x = 0∑Fy=0\sum F_y = 0∑MO=0\sum M_O = 0
  • Support Types and Reactive Unknowns:
    • Cable / Weightless Link: 1 unknown; directed in tension along the line of the cable/link.
    • Roller / Rocker / Smooth Surface: 1 unknown; contact force acting perpendicular to the surface.
    • Smooth Pin or Hinge: 2 unknowns; two orthogonal force components (AxA_x, AyA_y).
    • Fixed Connected Collar on Smooth Rod: 2 unknowns; force perpendicular to the rod and a resisting couple moment MM.
    • Fixed Support: 3 unknowns; two orthogonal force components (AxA_x, AyA_y) and a resisting couple moment (MAM_A).

Types of supports and reactions for rigid bodies

  • Reduction of Distributed Loads:
    • Equivalent Resultant Force (FRF_R): Equal to the total area underneath the distributed loading diagram w(x)w(x).
    • Uniform load of intensity ww over span LL:       FR=wLF_R = wL
    • Triangular load from 00 to peak intensity ww over span LL:       FR=12wLF_R = \frac{1}{2}wL
    • Line of Action (xˉ\bar{x}): Passes through the geometric centroid of the loading curve.
    • Triangle centroid is situated at 23L\frac{2}{3}L from the zero-load vertex (13L\frac{1}{3}L from the maximum base).

Centroid and resultant of a triangular distributed load

Internal Loadings and Beam Diagrams (SFD & BMD)

  • Components of Internal Loading:
    • Normal Force (NN): Acts perpendicular to the cut cross section.
    • Shear Force (VV): Acts tangent to the cut cross section.
    • Bending Moment (MM): Couple moment resisting bending at the cross section.
  • Internal Sign Convention:
    • Normal Force: Positive in tension (directed outward from the section).
    • Shear Force: Positive when causing clockwise rotation of the beam element (directed downward on the right-hand cut, upward on the left-hand cut).
    • Bending Moment: Positive when causing sagging / concave-upward curvature (compression at top, tension at bottom fibers).

Beam internal loadings sign convention

  • Method of Sections for Constructing Diagrams:
    • Find external support reactions using global rigid body equilibrium.
    • Establish position coordinates xx from the left end across discrete intervals separated by point loads, moments, or distributed load discontinuities.
    • Section beam at location xx, apply positive internal forces to the free-body diagram, and solve equilibrium equations to establish equations for V(x)V(x) and M(x)M(x).
    • Plot Shear Force Diagrams (SFD) and Bending Moment Diagrams (BMD); locations where the shear force passes through zero (V=0V = 0) define points of local maximum or minimum bending moment.

Shear force and bending moment diagrams for a triangular distributed load