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Propped cantilever with UDL by integration

Short answer

Prop reaction = 30 kN. Fixed-end vertical reaction = 50 kN, hogging moment = 40 kN·m. Maximum deflection = 1.73 mm downward at 2.31 m from fixed end. Point of contraflexure at 1 m from fixed end.

A cantilever of span 4 m fixed at A carries a uniformly distributed load of 20 kN/m over its whole length and is propped at the free end B so that B does not deflect. EI = 16 000 kN m^2 is constant. Using the double integration method find (a) the prop reaction, (b) the fixed-end reactions and moment, (c) the position and value of the maximum deflection, (d) the point of contraflexure.

Statically indeterminate beam

 ||A===================B
 ||  w = 20 kN/m       ^ R_B (prop)
 ||<------ 4 m ------>

Let RBR_B be the prop reaction. Take the origin at A, xx towards B, sagging moment positive and yy upward.

Let RA=wL−RBR_A = wL - R_B be the vertical reaction at the fixed end A, and MAM_A the hogging fixed-end moment. The bending moment at a section xx from A gives

EI y′′=RAx−MA−wx22EI\,y'' = R_Ax - M_A - \frac{wx^2}{2} EI y′=RAx22−MAx−wx36(C1=0 since y′=0 at x=0)EI\,y' = \frac{R_Ax^2}{2} - M_Ax - \frac{wx^3}{6} \quad (C_1=0\text{ since } y'=0\text{ at }x=0) EI y=RAx36−MAx22−wx424(C2=0 since y=0 at x=0)EI\,y = \frac{R_Ax^3}{6} - \frac{M_Ax^2}{2} - \frac{wx^4}{24} \quad (C_2=0\text{ since } y=0\text{ at }x=0)

(a) Prop reaction

Conditions: y=0y = 0 at x=Lx = L (prop), and M(L)=0M(L) = 0 at the free end B (no moment is applied there):

RAL−MA−wL22=0  ⇒  MA=RAL−wL22R_AL - M_A - \frac{wL^2}{2} = 0 \;\Rightarrow\; M_A = R_AL - \frac{wL^2}{2} EI yB=RAL36−MAL22−wL424=0EI\,y_B = \frac{R_AL^3}{6} - \frac{M_AL^2}{2} - \frac{wL^4}{24} = 0

Substituting MAM_A: RAL36−RAL32+wL44−wL424=0\dfrac{R_AL^3}{6} - \dfrac{R_AL^3}{2} + \dfrac{wL^4}{4} - \dfrac{wL^4}{24} = 0, hence RAL33=5wL424\dfrac{R_AL^3}{3} = \dfrac{5wL^4}{24}, so RA=5wL8R_A = \dfrac{5wL}{8}.

RA=5×20×48=50 kN,RB=wL−RA=80−50=30 kNR_A = \frac{5\times20\times4}{8} = 50\ \text{kN}, \qquad R_B = wL - R_A = 80 - 50 = 30\ \text{kN}

(b) Fixed-end reactions and moment

RA=50R_A = 50 kN (upward), and

MA=RAL−wL22=50×4−160=40 kN m (hogging)  (=wL28)M_A = R_AL - \frac{wL^2}{2} = 50\times4 - 160 = 40\ \text{kN m (hogging)} \;\left(=\frac{wL^2}{8}\right)

Check, moments about A: 30×4−80×2+40=030\times4 - 80\times2 + 40 = 0. ✓

(c) Maximum deflection (y′=0y'=0)

EI y′=25x2−40x−20x36=0  ⇒  3.333x2−25x+40=0EI\,y' = 25x^2 - 40x - \frac{20x^3}{6} = 0 \;\Rightarrow\; 3.333x^2 - 25x + 40 = 0 x=25−625−533.36.667=25−9.576.667=2.314 m (=0.5785L from A, i.e. 0.4215L from the prop)x = \frac{25 - \sqrt{625 - 533.3}}{6.667} = \frac{25 - 9.57}{6.667} = 2.314\ \text{m}\ (=0.5785L\text{ from A, i.e. }0.4215L\text{ from the prop}) EI y=50(2.314)36−40(2.314)22−20(2.314)424=103.2−107.1−23.9=−27.7EI\,y = \frac{50(2.314)^3}{6} - \frac{40(2.314)^2}{2} - \frac{20(2.314)^4}{24} = 103.2 - 107.1 - 23.9 = -27.7 ymax=−27.716000=−1.73×10−3 m=1.73 mm downwardy_{max} = \frac{-27.7}{16000} = -1.73\times10^{-3}\ \text{m} = 1.73\ \text{mm downward}

(d) Point of contraflexure

M(x)=50x−40−10x2=0⇒x2−5x+4=0⇒x=1 mM(x) = 50x - 40 - 10x^2 = 0 \Rightarrow x^2 - 5x + 4 = 0 \Rightarrow x = 1\ \text{m} or 4 m4\ \text{m}. The root x=4x = 4 m is the prop itself, so the point of contraflexure is at x=1x = 1 m from A. The maximum sagging moment is where V=0V = 0, at x=50/20=2.5x = 50/20 = 2.5 m: M=50(2.5)−40−10(6.25)=22.5M = 50(2.5) - 40 - 10(6.25) = 22.5 kN m.

Answer: RB=30R_B = 30 kN, RA=50R_A = 50 kN, MA=40M_A = 40 kN m; ymax=1.73y_{max} = 1.73 mm at 2.31 m from A; contraflexure at 1 m from A.

✓ Answer checked by Claude Opus 5.5 (high effort)

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