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Principal Stresses

Mechanics of Materials · FE Reference Handbook section

Mechanics of Materials
4 formulas
10 exam-style examples
~53 min
All Mechanics of Materials lectures

Handbook notes for this section

Definitions and conditions exactly as the handbook states them.

  • For the special case of a two-dimensional stress state, the equations for principal stress reduce to
  • this case. Depending on their values, the three roots are then labeled according to the convention:
  • indicated components shown in their positive sense.

Core formulas for this FE topic

Definitions, applicability, units, assumptions and worked examples for each relation.

Worked exam-style examples

The four ways this section is written on the real exam — thoughts first, then equations, then substitution.

Example 1
Flexural stress — solve for bending stress — Principal Stresses

A mechanics of materials problem uses Flexural stress. Given moment (M) = 1,790 kip·in; distance to extreme fiber (c) = 12.7000 in; moment of inertia (I) = 1,250 in⁴, determine the bending stress (sigma) in ksi.

Given

  • moment (M) = 1,790 kip·in

  • distancetoextremefiber(c)=12.7000indistance to extreme fiber (c) = 12.7000 in
  • momentofinertia(I)=1,250in4moment of inertia (I) = 1,250 in^{4}

Find

bending stress (sigma), in ksi

Start with the thinking

  • The governing relation printed in this handbook section is Flexural stress.
  • Everything except sigma is given, so isolate sigma symbolically first — never rearrange after the numbers are in.
  • Tabulate each given with its unit and confirm the units are consistent with the relation before substituting.
  • Mechanics of Materials items reward recognising the unknown before touching a calculator.

Step-by-step solution

  1. Step 1 — State the governing relation:

    σ=Mc/I\sigma = M c / I
  2. Step 2 — Rearrange the relation so that sigma stands alone on the left-hand side.

  3. Step 3 — List the givens: moment (M) = 1,790 kip·in, distance to extreme fiber (c) = 12.7000 in, moment of inertia (I) = 1,250 in⁴.

  4. Step 4 — Substitute the given values into the rearranged relation.

  5. Step 5 — Evaluate:

    σ=18.1864 ksi\sigma = 18.1864\ \text{ksi}
  6. Step 6 — Check: returning sigma = 18.1864 ksi to

    σ=Mc/I\sigma = M c / I

    reproduces the given quantities, and both sides carry the same units.

Answer:
σ=18.1864 ksi\sigma = 18.1864\ \text{ksi}

Why the other options are there

  • 36.3728 — kept a factor of two that cancels in the correct rearrangement.
  • 9.0932 — dropped that same factor in the other direction.
  • 20.0050 — rounded an intermediate value before the final step.

Reference: FE Reference Handbook — Mechanics of Materials → Principal Stresses

Example 2
Principal stresses (plane stress) — solve for max principal stress — Principal Stresses (2)

A shaft under combined bending and torsion is checked using principal stresses. Given normal stress x (sigma_x) = 5.0000 ksi; normal stress y (sigma_y) = -14.0000 ksi; shear stress (tau_xy) = 9.6000 ksi, determine the max principal stress (sigma_1) in ksi.

Given

  • normalstressx(sigmax)=5.0000ksinormal stress x (sigma_x) = 5.0000 ksi
  • normalstressy(sigmay)=−14.0000ksinormal stress y (sigma_y) = -14.0000 ksi
  • shearstress(tauxy)=9.6000ksishear stress (tau_xy) = 9.6000 ksi

Find

max principal stress (sigma_1), in ksi

Start with the thinking

  • The governing relation printed in this handbook section is Principal stresses (plane stress).
  • Everything except sigma_1 is given, so isolate sigma_1 symbolically first — never rearrange after the numbers are in.
  • Tabulate each given with its unit and confirm the units are consistent with the relation before substituting.
  • Principal stresses on a stressed element are the maximum and minimum normal stresses found from Mohr's circle relations.
\sigma_x\sigma_x\sigma_y\sigma_y\tau_{xy}Plane stress element

Figure 2 — schematic for Principal stresses (plane stress) — solve for max principal stress — Principal Stresses (2)

Step-by-step solution

  1. Step 1 — State the governing relation:

    σ1,2=σx+σy2±(σx−σy2)2+τxy2\sigma_{1,2} = \dfrac{\sigma_x+\sigma_y}{2} \pm \sqrt{\left(\dfrac{\sigma_x-\sigma_y}{2}\right)^2 + \tau_{xy}^2}
  2. Step 2 — Rearrange symbolically for sigma_1:

    σ1=σx+σy2+(σx−σy2)2+τxy2\sigma_{1} = \dfrac{\sigma_x+\sigma_y}{2} + \sqrt{\left(\dfrac{\sigma_x-\sigma_y}{2}\right)^2 + \tau_{xy}^2}
  3. Step 3 — List the givens: normal stress x (sigma_x) = 5.0000 ksi, normal stress y (sigma_y) = -14.0000 ksi, shear stress (tau_xy) = 9.6000 ksi.

  4. Step 4 — Substitute the given values:

    σ1=σx+σy2+(σx−σy2)2+9.60002\sigma_{1} = \dfrac{\sigma_x+\sigma_y}{2} + \sqrt{\left(\dfrac{\sigma_x-\sigma_y}{2}\right)^2 + 9.6000^2}
  5. Step 5 — Evaluate:

    σ1=9.0059 ksi\sigma_{1} = 9.0059\ \text{ksi}
  6. Step 6 — Check: returning sigma_1 = 9.0059 ksi to

    σ1,2=σx+σy2±(σx−σy2)2+τxy2\sigma_{1,2} = \dfrac{\sigma_x+\sigma_y}{2} \pm \sqrt{\left(\dfrac{\sigma_x-\sigma_y}{2}\right)^2 + \tau_{xy}^2}

    reproduces the given quantities, and both sides carry the same units.

Answer:
σ1=9.0059 ksi\sigma_{1} = 9.0059\ \text{ksi}

Why the other options are there

  • 18.0118 — kept a factor of two that cancels in the correct rearrangement.
  • 4.5030 — dropped that same factor in the other direction.
  • 9.9065 — rounded an intermediate value before the final step.

Reference: FE Handbook — Mechanics of Materials: Principal Stresses

Example 3
Flexural stress — solve for moment — Principal Stresses (3)

A mechanics of materials problem uses Flexural stress. Given distance to extreme fiber (c) = 14.3000 in; moment of inertia (I) = 580.0 in⁴; bending stress (sigma) = 21.3400 ksi, determine the moment (M) in kip·in.

Given

  • distancetoextremefiber(c)=14.3000indistance to extreme fiber (c) = 14.3000 in
  • momentofinertia(I)=580.0in4moment of inertia (I) = 580.0 in^{4}
  • bendingstress(sigma)=21.3400ksibending stress (sigma) = 21.3400 ksi

Find

moment (M), in kip·in

Start with the thinking

  • The governing relation printed in this handbook section is Flexural stress.
  • Everything except M is given, so isolate M symbolically first — never rearrange after the numbers are in.
  • Tabulate each given with its unit and confirm the units are consistent with the relation before substituting.
  • Mechanics of Materials items reward recognising the unknown before touching a calculator.

Step-by-step solution

  1. Step 1 — State the governing relation:

    σ=Mc/I\sigma = M c / I
  2. Step 2 — Rearrange the relation so that M stands alone on the left-hand side.

  3. Step 3 — List the givens: distance to extreme fiber (c) = 14.3000 in, moment of inertia (I) = 580.0 in⁴, bending stress (sigma) = 21.3400 ksi.

  4. Step 4 — Substitute the given values into the rearranged relation.

  5. Step 5 — Evaluate:

    M=865.5 kip⋅inM = 865.5\ \text{kip·in}
  6. Step 6 — Check: returning M = 865.5 kip·in to

    σ=Mc/I\sigma = M c / I

    reproduces the given quantities, and both sides carry the same units.

Answer:
M=865.5 kip⋅inM = 865.5\ \text{kip·in}

Why the other options are there

  • 1,731 — kept a factor of two that cancels in the correct rearrangement.
  • 432.8 — dropped that same factor in the other direction.
  • 952.1 — rounded an intermediate value before the final step.

Reference: FE Reference Handbook — Mechanics of Materials → Principal Stresses

Example 4
Principal stresses (plane stress) — solve for max principal stress (case 2) — Principal Stresses (4)

A plate with combined normal and shear stress is analyzed for principal stresses. Given normal stress x (sigma_x) = -18.0000 ksi; normal stress y (sigma_y) = -13.5000 ksi; shear stress (tau_xy) = 12.8000 ksi, determine the max principal stress (sigma_1) in ksi.

Given

  • normalstressx(sigmax)=−18.0000ksinormal stress x (sigma_x) = -18.0000 ksi
  • normalstressy(sigmay)=−13.5000ksinormal stress y (sigma_y) = -13.5000 ksi
  • shearstress(tauxy)=12.8000ksishear stress (tau_xy) = 12.8000 ksi

Find

max principal stress (sigma_1), in ksi

Start with the thinking

  • The governing relation printed in this handbook section is Principal stresses (plane stress).
  • Everything except sigma_1 is given, so isolate sigma_1 symbolically first — never rearrange after the numbers are in.
  • Tabulate each given with its unit and confirm the units are consistent with the relation before substituting.
  • Principal stresses on a stressed element are the maximum and minimum normal stresses found from Mohr's circle relations.
\sigma_x\sigma_x\sigma_y\sigma_y\tau_{xy}Plane stress element

Figure 4 — schematic for Principal stresses (plane stress) — solve for max principal stress (case 2) — Principal Stresses (4)

Step-by-step solution

  1. Step 1 — State the governing relation:

    σ1,2=σx+σy2±(σx−σy2)2+τxy2\sigma_{1,2} = \dfrac{\sigma_x+\sigma_y}{2} \pm \sqrt{\left(\dfrac{\sigma_x-\sigma_y}{2}\right)^2 + \tau_{xy}^2}
  2. Step 2 — Rearrange symbolically for sigma_1:

    σ1=σx+σy2+(σx−σy2)2+τxy2\sigma_{1} = \dfrac{\sigma_x+\sigma_y}{2} + \sqrt{\left(\dfrac{\sigma_x-\sigma_y}{2}\right)^2 + \tau_{xy}^2}
  3. Step 3 — List the givens: normal stress x (sigma_x) = -18.0000 ksi, normal stress y (sigma_y) = -13.5000 ksi, shear stress (tau_xy) = 12.8000 ksi.

  4. Step 4 — Substitute the given values:

    σ1=σx+σy2+(σx−σy2)2+12.80002\sigma_{1} = \dfrac{\sigma_x+\sigma_y}{2} + \sqrt{\left(\dfrac{\sigma_x-\sigma_y}{2}\right)^2 + 12.8000^2}
  5. Step 5 — Evaluate:

    σ1=−2.7538 ksi\sigma_{1} = -2.7538\ \text{ksi}
  6. Step 6 — Check: returning sigma_1 = -2.7538 ksi to

    σ1,2=σx+σy2±(σx−σy2)2+τxy2\sigma_{1,2} = \dfrac{\sigma_x+\sigma_y}{2} \pm \sqrt{\left(\dfrac{\sigma_x-\sigma_y}{2}\right)^2 + \tau_{xy}^2}

    reproduces the given quantities, and both sides carry the same units.

Answer:
σ1=−2.7538 ksi\sigma_{1} = -2.7538\ \text{ksi}

Why the other options are there

  • -5.5075 — kept a factor of two that cancels in the correct rearrangement.
  • -1.3769 — dropped that same factor in the other direction.
  • -3.0291 — rounded an intermediate value before the final step.

Reference: FE Handbook — Mechanics of Materials: Principal Stresses

Example 5
Flexural stress — solve for distance to extreme fiber — Principal Stresses (5)

A mechanics of materials problem uses Flexural stress. Given moment (M) = 2,860 kip·in; moment of inertia (I) = 190.0 in⁴; bending stress (sigma) = 48.7600 ksi, determine the distance to extreme fiber (c) in in.

Given

  • moment (M) = 2,860 kip·in

  • momentofinertia(I)=190.0in4moment of inertia (I) = 190.0 in^{4}
  • bendingstress(sigma)=48.7600ksibending stress (sigma) = 48.7600 ksi

Find

distance to extreme fiber (c), in in

Start with the thinking

  • The governing relation printed in this handbook section is Flexural stress.
  • Everything except c is given, so isolate c symbolically first — never rearrange after the numbers are in.
  • Tabulate each given with its unit and confirm the units are consistent with the relation before substituting.
  • Mechanics of Materials items reward recognising the unknown before touching a calculator.

Step-by-step solution

  1. Step 1 — State the governing relation:

    σ=Mc/I\sigma = M c / I
  2. Step 2 — Rearrange the relation so that c stands alone on the left-hand side.

  3. Step 3 — List the givens: moment (M) = 2,860 kip·in, moment of inertia (I) = 190.0 in⁴, bending stress (sigma) = 48.7600 ksi.

  4. Step 4 — Substitute the given values into the rearranged relation.

  5. Step 5 — Evaluate:

    c=3.2393 inc = 3.2393\ \text{in}
  6. Step 6 — Check: returning c = 3.2393 in to

    σ=Mc/I\sigma = M c / I

    reproduces the given quantities, and both sides carry the same units.

Answer:
c=3.2393 inc = 3.2393\ \text{in}

Why the other options are there

  • 6.4786 — kept a factor of two that cancels in the correct rearrangement.
  • 1.6197 — dropped that same factor in the other direction.
  • 3.5632 — rounded an intermediate value before the final step.

Reference: FE Reference Handbook — Mechanics of Materials → Principal Stresses

Example 6
Principal stresses (plane stress) — solve for max principal stress (case 3) — Principal Stresses (6)

A pressure vessel wall's principal stresses are computed from biaxial loading. Given normal stress x (sigma_x) = -14.5000 ksi; normal stress y (sigma_y) = 8.0000 ksi; shear stress (tau_xy) = 7.8000 ksi, determine the max principal stress (sigma_1) in ksi.

Given

  • normalstressx(sigmax)=−14.5000ksinormal stress x (sigma_x) = -14.5000 ksi
  • normalstressy(sigmay)=8.0000ksinormal stress y (sigma_y) = 8.0000 ksi
  • shearstress(tauxy)=7.8000ksishear stress (tau_xy) = 7.8000 ksi

Find

max principal stress (sigma_1), in ksi

Start with the thinking

  • The governing relation printed in this handbook section is Principal stresses (plane stress).
  • Everything except sigma_1 is given, so isolate sigma_1 symbolically first — never rearrange after the numbers are in.
  • Tabulate each given with its unit and confirm the units are consistent with the relation before substituting.
  • Principal stresses on a stressed element are the maximum and minimum normal stresses found from Mohr's circle relations.
\sigma_x\sigma_x\sigma_y\sigma_y\tau_{xy}Plane stress element

Figure 6 — schematic for Principal stresses (plane stress) — solve for max principal stress (case 3) — Principal Stresses (6)

Step-by-step solution

  1. Step 1 — State the governing relation:

    σ1,2=σx+σy2±(σx−σy2)2+τxy2\sigma_{1,2} = \dfrac{\sigma_x+\sigma_y}{2} \pm \sqrt{\left(\dfrac{\sigma_x-\sigma_y}{2}\right)^2 + \tau_{xy}^2}
  2. Step 2 — Rearrange symbolically for sigma_1:

    σ1=σx+σy2+(σx−σy2)2+τxy2\sigma_{1} = \dfrac{\sigma_x+\sigma_y}{2} + \sqrt{\left(\dfrac{\sigma_x-\sigma_y}{2}\right)^2 + \tau_{xy}^2}
  3. Step 3 — List the givens: normal stress x (sigma_x) = -14.5000 ksi, normal stress y (sigma_y) = 8.0000 ksi, shear stress (tau_xy) = 7.8000 ksi.

  4. Step 4 — Substitute the given values:

    σ1=σx+σy2+(σx−σy2)2+7.80002\sigma_{1} = \dfrac{\sigma_x+\sigma_y}{2} + \sqrt{\left(\dfrac{\sigma_x-\sigma_y}{2}\right)^2 + 7.8000^2}
  5. Step 5 — Evaluate:

    σ1=10.4395 ksi\sigma_{1} = 10.4395\ \text{ksi}
  6. Step 6 — Check: returning sigma_1 = 10.4395 ksi to

    σ1,2=σx+σy2±(σx−σy2)2+τxy2\sigma_{1,2} = \dfrac{\sigma_x+\sigma_y}{2} \pm \sqrt{\left(\dfrac{\sigma_x-\sigma_y}{2}\right)^2 + \tau_{xy}^2}

    reproduces the given quantities, and both sides carry the same units.

Answer:
σ1=10.4395 ksi\sigma_{1} = 10.4395\ \text{ksi}

Why the other options are there

  • 20.8790 — kept a factor of two that cancels in the correct rearrangement.
  • 5.2198 — dropped that same factor in the other direction.
  • 11.4835 — rounded an intermediate value before the final step.

Reference: FE Handbook — Mechanics of Materials: Principal Stresses

Example 7
Flexural stress — solve for moment of inertia — Principal Stresses (7)

A mechanics of materials problem uses Flexural stress. Given moment (M) = 2,590 kip·in; distance to extreme fiber (c) = 11.2000 in; bending stress (sigma) = 6.9800 ksi, determine the moment of inertia (I) in in⁴.

Given

  • moment (M) = 2,590 kip·in

  • distancetoextremefiber(c)=11.2000indistance to extreme fiber (c) = 11.2000 in
  • bendingstress(sigma)=6.9800ksibending stress (sigma) = 6.9800 ksi

Find

moment of inertia (I), in in⁴

Start with the thinking

  • The governing relation printed in this handbook section is Flexural stress.
  • Everything except I is given, so isolate I symbolically first — never rearrange after the numbers are in.
  • Tabulate each given with its unit and confirm the units are consistent with the relation before substituting.
  • Mechanics of Materials items reward recognising the unknown before touching a calculator.

Step-by-step solution

  1. Step 1 — State the governing relation:

    σ=Mc/I\sigma = M c / I
  2. Step 2 — Rearrange the relation so that I stands alone on the left-hand side.

  3. Step 3 — List the givens: moment (M) = 2,590 kip·in, distance to extreme fiber (c) = 11.2000 in, bending stress (sigma) = 6.9800 ksi.

  4. Step 4 — Substitute the given values into the rearranged relation.

  5. Step 5 — Evaluate:

    I=4156 in⁴I = 4156\ \text{in⁴}
  6. Step 6 — Check: returning I = 4,156 in⁴ to

    σ=Mc/I\sigma = M c / I

    reproduces the given quantities, and both sides carry the same units.

Answer:
I=4156 in⁴I = 4156\ \text{in⁴}

Why the other options are there

  • 8,312 — kept a factor of two that cancels in the correct rearrangement.
  • 2,078 — dropped that same factor in the other direction.
  • 4,571 — rounded an intermediate value before the final step.

Reference: FE Reference Handbook — Mechanics of Materials → Principal Stresses

Example 8
Principal stresses (plane stress) — solve for max principal stress (case 4) — Principal Stresses (8)

A shaft under combined bending and torsion is checked using principal stresses. Given normal stress x (sigma_x) = 8.0000 ksi; normal stress y (sigma_y) = 0.0000 ksi; shear stress (tau_xy) = 14.6000 ksi, determine the max principal stress (sigma_1) in ksi.

Given

  • normalstressx(sigmax)=8.0000ksinormal stress x (sigma_x) = 8.0000 ksi
  • normalstressy(sigmay)=0.0000ksinormal stress y (sigma_y) = 0.0000 ksi
  • shearstress(tauxy)=14.6000ksishear stress (tau_xy) = 14.6000 ksi

Find

max principal stress (sigma_1), in ksi

Start with the thinking

  • The governing relation printed in this handbook section is Principal stresses (plane stress).
  • Everything except sigma_1 is given, so isolate sigma_1 symbolically first — never rearrange after the numbers are in.
  • Tabulate each given with its unit and confirm the units are consistent with the relation before substituting.
  • Principal stresses on a stressed element are the maximum and minimum normal stresses found from Mohr's circle relations.
\sigma_x\sigma_x\sigma_y\sigma_y\tau_{xy}Plane stress element

Figure 8 — schematic for Principal stresses (plane stress) — solve for max principal stress (case 4) — Principal Stresses (8)

Step-by-step solution

  1. Step 1 — State the governing relation:

    σ1,2=σx+σy2±(σx−σy2)2+τxy2\sigma_{1,2} = \dfrac{\sigma_x+\sigma_y}{2} \pm \sqrt{\left(\dfrac{\sigma_x-\sigma_y}{2}\right)^2 + \tau_{xy}^2}
  2. Step 2 — Rearrange symbolically for sigma_1:

    σ1=σx+σy2+(σx−σy2)2+τxy2\sigma_{1} = \dfrac{\sigma_x+\sigma_y}{2} + \sqrt{\left(\dfrac{\sigma_x-\sigma_y}{2}\right)^2 + \tau_{xy}^2}
  3. Step 3 — List the givens: normal stress x (sigma_x) = 8.0000 ksi, normal stress y (sigma_y) = 0.0000 ksi, shear stress (tau_xy) = 14.6000 ksi.

  4. Step 4 — Substitute the given values:

    σ1=σx+σy2+(σx−σy2)2+14.60002\sigma_{1} = \dfrac{\sigma_x+\sigma_y}{2} + \sqrt{\left(\dfrac{\sigma_x-\sigma_y}{2}\right)^2 + 14.6000^2}
  5. Step 5 — Evaluate:

    σ1=19.1380 ksi\sigma_{1} = 19.1380\ \text{ksi}
  6. Step 6 — Check: returning sigma_1 = 19.1380 ksi to

    σ1,2=σx+σy2±(σx−σy2)2+τxy2\sigma_{1,2} = \dfrac{\sigma_x+\sigma_y}{2} \pm \sqrt{\left(\dfrac{\sigma_x-\sigma_y}{2}\right)^2 + \tau_{xy}^2}

    reproduces the given quantities, and both sides carry the same units.

Answer:
σ1=19.1380 ksi\sigma_{1} = 19.1380\ \text{ksi}

Why the other options are there

  • 38.2761 — kept a factor of two that cancels in the correct rearrangement.
  • 9.5690 — dropped that same factor in the other direction.
  • 21.0518 — rounded an intermediate value before the final step.

Reference: FE Handbook — Mechanics of Materials: Principal Stresses

Example 9
Flexural stress — solve for bending stress (case 2) — Principal Stresses (9)

A mechanics of materials problem uses Flexural stress. Given moment (M) = 3,800 kip·in; distance to extreme fiber (c) = 5.0000 in; moment of inertia (I) = 920.0 in⁴, determine the bending stress (sigma) in ksi.

Given

  • moment (M) = 3,800 kip·in

  • distancetoextremefiber(c)=5.0000indistance to extreme fiber (c) = 5.0000 in
  • momentofinertia(I)=920.0in4moment of inertia (I) = 920.0 in^{4}

Find

bending stress (sigma), in ksi

Start with the thinking

  • The governing relation printed in this handbook section is Flexural stress.
  • Everything except sigma is given, so isolate sigma symbolically first — never rearrange after the numbers are in.
  • Tabulate each given with its unit and confirm the units are consistent with the relation before substituting.
  • Mechanics of Materials items reward recognising the unknown before touching a calculator.

Step-by-step solution

  1. Step 1 — State the governing relation:

    σ=Mc/I\sigma = M c / I
  2. Step 2 — Rearrange the relation so that sigma stands alone on the left-hand side.

  3. Step 3 — List the givens: moment (M) = 3,800 kip·in, distance to extreme fiber (c) = 5.0000 in, moment of inertia (I) = 920.0 in⁴.

  4. Step 4 — Substitute the given values into the rearranged relation.

  5. Step 5 — Evaluate:

    σ=20.6522 ksi\sigma = 20.6522\ \text{ksi}
  6. Step 6 — Check: returning sigma = 20.6522 ksi to

    σ=Mc/I\sigma = M c / I

    reproduces the given quantities, and both sides carry the same units.

Answer:
σ=20.6522 ksi\sigma = 20.6522\ \text{ksi}

Why the other options are there

  • 41.3043 — kept a factor of two that cancels in the correct rearrangement.
  • 10.3261 — dropped that same factor in the other direction.
  • 22.7174 — rounded an intermediate value before the final step.

Reference: FE Reference Handbook — Mechanics of Materials → Principal Stresses

Example 10
Principal stresses (plane stress) — solve for max principal stress (case 5) — Principal Stresses (10)

A plate with combined normal and shear stress is analyzed for principal stresses. Given normal stress x (sigma_x) = -19.0000 ksi; normal stress y (sigma_y) = -10.5000 ksi; shear stress (tau_xy) = 12.0000 ksi, determine the max principal stress (sigma_1) in ksi.

Given

  • normalstressx(sigmax)=−19.0000ksinormal stress x (sigma_x) = -19.0000 ksi
  • normalstressy(sigmay)=−10.5000ksinormal stress y (sigma_y) = -10.5000 ksi
  • shearstress(tauxy)=12.0000ksishear stress (tau_xy) = 12.0000 ksi

Find

max principal stress (sigma_1), in ksi

Start with the thinking

  • The governing relation printed in this handbook section is Principal stresses (plane stress).
  • Everything except sigma_1 is given, so isolate sigma_1 symbolically first — never rearrange after the numbers are in.
  • Tabulate each given with its unit and confirm the units are consistent with the relation before substituting.
  • Principal stresses on a stressed element are the maximum and minimum normal stresses found from Mohr's circle relations.
\sigma_x\sigma_x\sigma_y\sigma_y\tau_{xy}Plane stress element

Figure 10 — schematic for Principal stresses (plane stress) — solve for max principal stress (case 5) — Principal Stresses (10)

Step-by-step solution

  1. Step 1 — State the governing relation:

    σ1,2=σx+σy2±(σx−σy2)2+τxy2\sigma_{1,2} = \dfrac{\sigma_x+\sigma_y}{2} \pm \sqrt{\left(\dfrac{\sigma_x-\sigma_y}{2}\right)^2 + \tau_{xy}^2}
  2. Step 2 — Rearrange symbolically for sigma_1:

    σ1=σx+σy2+(σx−σy2)2+τxy2\sigma_{1} = \dfrac{\sigma_x+\sigma_y}{2} + \sqrt{\left(\dfrac{\sigma_x-\sigma_y}{2}\right)^2 + \tau_{xy}^2}
  3. Step 3 — List the givens: normal stress x (sigma_x) = -19.0000 ksi, normal stress y (sigma_y) = -10.5000 ksi, shear stress (tau_xy) = 12.0000 ksi.

  4. Step 4 — Substitute the given values:

    σ1=σx+σy2+(σx−σy2)2+12.00002\sigma_{1} = \dfrac{\sigma_x+\sigma_y}{2} + \sqrt{\left(\dfrac{\sigma_x-\sigma_y}{2}\right)^2 + 12.0000^2}
  5. Step 5 — Evaluate:

    σ1=−2.0196 ksi\sigma_{1} = -2.0196\ \text{ksi}
  6. Step 6 — Check: returning sigma_1 = -2.0196 ksi to

    σ1,2=σx+σy2±(σx−σy2)2+τxy2\sigma_{1,2} = \dfrac{\sigma_x+\sigma_y}{2} \pm \sqrt{\left(\dfrac{\sigma_x-\sigma_y}{2}\right)^2 + \tau_{xy}^2}

    reproduces the given quantities, and both sides carry the same units.

Answer:
σ1=−2.0196 ksi\sigma_{1} = -2.0196\ \text{ksi}

Why the other options are there

  • -4.0392 — kept a factor of two that cancels in the correct rearrangement.
  • -1.0098 — dropped that same factor in the other direction.
  • -2.2216 — rounded an intermediate value before the final step.

Reference: FE Handbook — Mechanics of Materials: Principal Stresses

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