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Mechanics of Materials

From transcript: 20ME340 Mechanics of Materials (E) · 20ME48L Basic Material Testing (A)

Cheat sheet

Printable study sheet: formulas → definitions → topic notes → traps.

Formulas

Axial: σ = P/A ; δ = PL/(AE) ; thermal δ = α L ΔT ; total δ = mechanical + thermal
Torsion (circular): τ/r = T/J = Gθ/L ; J_solid = π d⁴/64 ; J_hollow = π(Do⁴−Di⁴)/64
Bending: σ = M y / I ; max at outer fiber; neutral axis through centroid
Shear in beams: τ = V Q /(I b) ; rectangular max = 1.5 V/A at NA
Combined: Mohr’s circle; σ_{1,2} = σx/2 ± √((σx/2)²+τ²) for plane stress σy=0
Hooke: σ = E ε ; γ = τ/G ; ε_lat = −ν ε_long ; E = 2G(1+ν)
Strain energy axial U = P²L/(2AE) ; torsion U = T²L/(2GJ)
Euler buckling: Pcr = π² E I / (K L)² ; K pinned-pinned=1; fixed-free=2; fixed-fixed=0.5; fixed-pinned≈0.7
Slenderness λ = K L / k ; k=√(I/A)
Max shear theory (Tresca): τ_max ≤ Sy/2 ; von Mises: √(σ1²+σ2²+σ3²−σ1σ2−…) ≤ Sy
Fatigue Goodman: σa/Se + σm/Sut ≤ 1/n ; Soderberg uses Sy for mean
Stress concentration: σ_max = Kt σ_nom
Pressure vessel thin: hoop σθ = p r / t ; long. σz = p r /(2t)
σ = P/A ; ε = δ/L ; E = σ/ε (elastic)
δ = PL/(AE)
Bending: σ = My/I ; τ = VQ/(Ib)
Torsion (round): τ = Tr/J ; θ = TL/(GJ)
Combined: Mohr's circle — principal σ1,2 = σx/2 ± √((σx/2)²+τ²)
Euler buckling: Pcr = π²EI/(KL)²

Definitions

Elastic limit / yield
Onset of permanent set; Sy used in ductile design
Ultimate strength Sut
Max engineering stress on curve
Modulus E
Slope of elastic σ–ε ; stiffness of material
Poisson ν
−ε_lat/ε_long ; metals ~0.3
Section modulus Z
I/y_max — bending strength geometric measure
Principal stress
Normal stresses on planes of zero shear
Stiffness vs strength
Deflection resistance vs load to fail
Buckling
Sudden lateral instability of compressed slender members
Endurance limit Se
Stress amplitude for infinite life (steels often)
Factor of safety n
Strength / allowable working stress
Stress / strain
Internal force intensity / relative deformation
Yield strength
Onset of permanent deformation (design often uses Sy/n)

Topic-wise short notes

Study these first — one block per syllabus topic. Then read the deep notes below.

Axial, bending, torsion

  • Statically indeterminate axial: compatibility of δ + equilibrium.
  • Beams: draw V & M first; σ_b from M; deflection via EI y''=M.
  • Double integration, Macaulay, moment-area, energy (Castigliano) methods.
  • Unsymmetric bending: resolve about principal axes of inertia.
  • Shear center: point where load causes bending without twist.

Failure theories

  • Ductile → Tresca (conservative) or von Mises (better match).
  • Brittle → max normal stress theory.
  • Mohr’s theory for different tension/compression strengths.
  • Always state which theory and why material class.

Axial, torsion, thermal

  • Bars in series: same P, δ sum; parallel: same δ, P sum.
  • Composite shafts: θ same if joined; share T by GJ stiffness.

Beams & buckling

  • Boundary K factors dominate Pcr — fixity is design.
  • Intermediate columns: Rankine/Gordon empirical vs pure Euler.
  • Kt at fillets, keyways, holes — use charts; fatigue sensitive.

Failure theories & fatigue

  • Infinite life if σa below Se (adjusted); else finite life via S–N.
  • Mean stress tensile hurts fatigue; compressive mean often less harmful.
  • Miner's rule for variable amplitude cumulative damage (approx).

Pressure vessels & combined loading

  • Thin wall: hoop = pr/t, long = pr/(2t); thick wall Lame equations.
  • Combined axial+bending+torsion → Mohr or principals then failure theory.
  • Thermal stress when δ_thermal prevented: σ=EαΔT (fixed ends).

Exam traps & quick notes

Comprehensive notes

Axial, bending, torsion

Superposition for combined loading; neutral axis; shear flow in thin walls.

Failure theories

Max normal (brittle), Tresca & von Mises (ductile). Fatigue: S–N, endurance limit, Goodman/Soderberg.

Axial, torsion, thermal

δ=PL/AE; thermal δ=αLΔT; torsion τ=Tr/J, θ=TL/GJ for circular shafts. Combined loading → principal stresses via Mohr.

Beams & buckling

σ=My/I; shear flow; deflection methods (double integration, energy). Euler buckling Pcr=π²EI/(KL)² with end-condition K. Stress concentrations Kt at fillets/holes.

Failure theories & fatigue

Ductile: Tresca/von Mises. Brittle: max normal. Fatigue: S–N, endurance limit, mean stress (Goodman). Design for infinite life vs finite life.

Interview Q&A for this subject

Q: Where is bending stress max in a cantilever with end load?
A: At the fixed root outer fibers — M is max at support.