Equivalent Nodal Forces

When deriving the formulation, IVW = EVW, simply we assumed that there is only nodal forces and that’s why EVW = δ 𝐪 𝖳 𝐏 . Now suppose that there are body forces and surface traction.

Let 𝐛 : body force per unit mass 𝐭 ¯ : prescribed boundary force or surface traction per unit area. (here I have used a bar over the traction vector to indicate that it is a prescribed one)

Then E V W = Ω ρ 𝐛 δ 𝐮 d V + Γ t 𝐭 ¯ δ 𝐮 d S + δ 𝐪 𝖳 𝐏 which can be written as E V W = Ω ρ δ 𝐮 𝖳 𝐛 d V + Γ t δ 𝐮 𝖳   𝐭 ¯ d S + δ 𝐪 𝖳 𝐏 However, δ 𝐮 = 𝐍   δ 𝐪 or { u } = [ N ] { δ q } Therefore, \begin{aligned} EVW&= \int_\Omega \rho\, \delta \mathbf{q}^{\mathsf T} \mathbf{N}^{\mathsf T} \mathbf{b}\, dV+\int_\Gamma \delta\mathbf{q}^{\mathsf T}\mathbf{N}^{\mathsf T}\bar{\mathbf{t}}\, dS+\delta\mathbf{q}^{\mathsf T}\mathbf{P}\\ &=\delta \mathbf{q}^{\mathsf T} \left(\int_\Omega \rho\, \mathbf{N}^{\mathsf T} \mathbf{b}\, dV+\int_\Gamma \mathbf{N}^{\mathsf T}\bar{\mathbf{t}}\, dS+\mathbf{P}\right) \end{aligned}

Equating EVW = IVW gives us 𝐊 𝐪 = 𝐅 where 𝐊 = Ω 𝐁 𝖳 𝐄 𝐁 d V and 𝐅 = Ω ρ 𝐍 𝖳 𝐛 d V + Γ 𝐍 𝖳 𝐭 ¯ d S + 𝐏

Example: If the beam is loaded as in the following figure,

Illustration for Equivalent Nodal Forces

then t ¯ ( x ) = w L x and the equivalent generalized nodal forces are: P 1 = 0 L N 1 ( x ) t ¯ ( x ) d x = 3 w L 20 M 1 = 0 L N 2 ( x ) t ¯ ( x ) d x = w L 2 30 P 2 = 0 L N 3 ( x ) t ¯ ( x ) d x = 7 w L 20 M 2 = 0 L N 4 ( x ) t ¯ ( x ) d x = w L 2 20 where \begin{aligned} N_1(x) &= 1 - \frac{3x^2}{L^2} + \frac{2x^3}{L^3} \\ N_2(x) &= x - \frac{2x^2}{L} + \frac{x^3}{L^2} \\ N_3(x) &= \frac{3x^2}{L^2} - \frac{2x^3}{L^3} \\ N_4(x) &= -\frac{x^2}{L} + \frac{x^3}{L^2} \end{aligned}

Illustration for Equivalent Nodal Forces