Formula Library
Searchable database of governing structural design equations, each with variables, assumptions, code reference, and links to worked examples.
Axial Tension
Yielding on gross section
phi_t P_n = 0.90 · F_y · A_g
Variables
- F_y — specified minimum yield stress (ksi)
- A_g — gross cross-sectional area (in²)
Assumptions
- Load applied along member axis
- No initial imperfections considered
AISC 360-22 §D2(a)Worked example → wx-4-1
Axial Tension
Rupture on effective net area
phi_t P_n = 0.75 · F_u · A_e
Variables
- F_u — specified minimum tensile strength (ksi)
- A_e — effective net area = U·A_n (in²)
Assumptions
- A_n uses d_h = d_b + 1/8
- Shear-lag factor U per Table D3.1
AISC 360-22 §D2(b)
Compression
Compressive strength (flexural buckling)
phi_c P_n = 0.90 · F_cr · A_g
Variables
- F_cr — critical stress (Eq E3-2 or E3-3) (ksi)
- A_g — gross area (in²)
Assumptions
- Members without slender elements
- Effective length factor K assumed known
AISC 360-22 §E3
Flexure
Plastic moment capacity
phi_b M_p = 0.90 · F_y · Z_x
Variables
- Z_x — plastic section modulus about x-axis (in³)
Assumptions
- Compact section (λ ≤ λ_p)
- Full lateral bracing (L_b ≤ L_p)
AISC 360-22 §F2.1
Shear
Shear strength of W-shape webs
phi_v V_n = 1.00 · 0.6 · F_y · A_w · C_v1
Variables
- A_w — web area = d · t_w (in²)
- C_v1 — web shear strength coefficient (—)
Assumptions
- Rolled I-shapes with h/t_w ≤ 2.24√(E/Fy) give C_v1 = 1.0
AISC 360-22 §G2.1
Torsion
Torsional strength of HSS
phi_T T_n = 0.90 · F_cr · C
Variables
- C — HSS torsional constant (in³)
- F_cr — critical torsional stress (ksi)
Assumptions
- Closed HSS section
- Ends free to warp
AISC 360-22 §H3.1
Combined Loading
Beam-column interaction (H1-1a)
P_r/P_c + 8/9 · (M_rx/M_cx + M_ry/M_cy) ≤ 1.0 (P_r/P_c ≥ 0.2)
Variables
- P_r — required axial (kips)
- P_c — available axial (kips)
- M_r — required moment (k·ft)
- M_c — available moment (k·ft)
Assumptions
- Doubly symmetric section
- Elastic second-order effects included in P_r, M_r
AISC 360-22 §H1.1
Connections
Bolt shear strength
phi R_n = 0.75 · F_nv · A_b
Variables
- F_nv — nominal shear stress (Table J3.2) (ksi)
- A_b — nominal bolt area (in²)
Assumptions
- Threads in shear plane → F_nv = 54 ksi for A325
AISC 360-22 §J3.6
Deflection
Midspan deflection (simple beam, UDL)
Δ_max = 5·w·L^4 / (384·E·I)
Variables
- w — uniform load (k/in)
- L — span (in)
- E — modulus of elasticity (ksi)
- I — moment of inertia (in⁴)
Assumptions
- Simply supported
- Elastic behaviour
Mechanics of Materials
Stability
Euler buckling load
P_e = π² · E · I / (K · L)²
Variables
- K — effective length factor (—)
- L — unbraced length (in)
Assumptions
- Perfectly straight, elastic, pin-ended column
AISC 360-22 §E3 Commentary