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Resultant stress on planes EF and GE, principal stresses

Short answer

Resolve 50 MN/m² on EF: σn = 50 cos30° = 43.30 MN/m², τ = 25 MN/m². With σ on GE = 30 MN/m², τxy = 25. Resultant on GE = √(30²+25²) = 39.05 MN/m² at 39.8° to normal. Principal stresses = 62.52 and 10.78 MN/m²; planes at 37.55° to EF normal. τmax = 25.87 MN/m².

At a point in a material under stress, the intensity of resultant stress on a plane EF is 50 MN/m250\ \text{MN/m}^2 (tensile) inclined at 30∘30^\circ to the normal to that plane. The stress on another plane at right angles to this plane is 30 MN/m230\ \text{MN/m}^2. Determine: (i) The resultant stress on the plane GE. (ii) The principal stresses and the principle planes. (iii) Maximum shear stress and its plane. [Figure: a corner of the material with plane GE horizontal (stress of 30 MN/m230\ \text{MN/m}^2 acting upward on it) and plane EF vertical (resultant stress 50 acting at 30∘30^\circ to the normal to EF).]

Assumption: the 30 MN/m² on plane GE is the normal (tensile) stress on it, as in the figure. Shear stresses on two perpendicular planes are equal in magnitude, so the shear on GE equals the shear on EF.

Components on plane EF

The 50 MN/m² resultant is at 30∘30^\circ to the normal of EF:

σEF=50cos⁡30∘=43.30 MN/m2,τEF=50sin⁡30∘=25.00 MN/m2\sigma_{EF} = 50\cos 30^\circ = 43.30\ \text{MN/m}^2, \qquad \tau_{EF} = 50\sin 30^\circ = 25.00\ \text{MN/m}^2

On the perpendicular plane GE: σGE=30\sigma_{GE} = 30 and τGE=25.00\tau_{GE} = 25.00 MN/m².

So σx=43.30\sigma_x = 43.30, σy=30\sigma_y = 30, τxy=25.00\tau_{xy} = 25.00 (all in MN/m²).

(i) Resultant stress on plane GE

σR=302+25.002=39.05 MN/m2,tan⁡α=25.0030⇒α=39.81∘ to the normal of GE\sigma_R = \sqrt{30^2 + 25.00^2} = 39.05\ \text{MN/m}^2, \qquad \tan\alpha = \frac{25.00}{30} \Rightarrow \alpha = 39.81^\circ\ \text{to the normal of GE}

(ii) Principal stresses and planes

σ1,2=43.30+302±(43.30−302)2+25.002=36.65±25.87\sigma_{1,2} = \frac{43.30+30}{2} \pm \sqrt{\left(\frac{43.30-30}{2}\right)^2 + 25.00^2} = 36.65 \pm 25.87 σ1=62.52 MN/m2,σ2=10.78 MN/m2\sigma_1 = 62.52\ \text{MN/m}^2, \qquad \sigma_2 = 10.78\ \text{MN/m}^2 tan⁡2θp=2(25)43.30−30⇒2θp=75.10∘, θp=37.55∘\tan 2\theta_p = \frac{2(25)}{43.30-30} \Rightarrow 2\theta_p = 75.10^\circ,\ \theta_p = 37.55^\circ

σ1\sigma_1 acts on the plane whose normal is at 37.55∘37.55^\circ to the normal of EF; σ2\sigma_2 acts on the plane at 127.55∘127.55^\circ (both planes are at right angles).

(iii) Maximum shear stress

τmax=σ1−σ22=25.87 MN/m2\tau_{max} = \frac{\sigma_1-\sigma_2}{2} = 25.87\ \text{MN/m}^2

It acts on planes at 45∘45^\circ to the principal planes, i.e. at 82.55∘82.55^\circ and 172.55∘172.55^\circ from the normal of EF, with a normal stress of 36.6536.65 MN/m² on them.

✓ Answer checked by Claude Opus 5.5 (high effort)

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