Resources Numerical accuracy
Calculations
Every calculation under our calculation policies: what it works out, its formula and the precision it runs at. Open one to see its code as it is in the released app.
Calculations
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Tension resistance
The design tension resistance of the gross section, and of the net section when one is given.
Nt,Rd = min(A fy ÷ γM0, 0.9 A_net fu ÷ γM2)
Steel member resistance to EN 1993-1-1 frame/frame-design-en.js64-bit- CadCraft
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Shear resistance along the web
The plastic shear resistance, and the shear buckling resistance of a slender web.
Vpl,Rd = Av fy ÷ (√3 γM0); λ̄w = hw ÷ (86.4 tw ε); χw = η or 0.83 ÷ λ̄w
Steel member resistance to EN 1993-1-1 frame/frame-design-en.js64-bit- CadCraft
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Bending resistance with high shear
The major-axis bending resistance reduced when the shear exceeds half the plastic shear resistance.
ρ = (2 V_Ed ÷ Vpl,Rd − 1)²; W = Wpl,y − ρ Aw² ÷ (4 tw)
Steel member resistance to EN 1993-1-1 frame/frame-design-en.js64-bit- CadCraft
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Bending and axial force on the cross-section
The utilization of the cross-section under axial force and bending about both axes.
class 1–2: (My ÷ M_N,y)² + (Mz ÷ M_N,z)^β, β = max(5n, 1); class 3: σ ÷ (fy ÷ γM0)
Steel member resistance to EN 1993-1-1 frame/frame-design-en.js64-bit- CadCraft
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Buckling reduction factor
The reduction factor χ for a slenderness and a buckling curve.
Φ = 0.5 (1 + α (λ̄ − 0.2) + λ̄²); χ = 1 ÷ (Φ + √(Φ² − λ̄²)) ≤ 1
Steel member resistance to EN 1993-1-1 frame/frame-design-en.js64-bit- CadCraft
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Buckling resistance in compression
The design buckling resistance for flexural buckling about both axes and torsional buckling.
Ncr = π² E I ÷ L²; λ̄ = √(A fy ÷ Ncr); Nb,Rd = χ A fy ÷ γM1
Steel member resistance to EN 1993-1-1 frame/frame-design-en.js64-bit- CadCraft
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Lateral-torsional buckling resistance
The design bending resistance of an unrestrained segment.
Mcr = C1 (π² E Iz ÷ L²) √(Iw ÷ Iz + L² G It ÷ (π² E Iz)); λ̄LT = √(W fy ÷ Mcr); Mb,Rd = χLT W fy ÷ γM1
Steel member resistance to EN 1993-1-1 frame/frame-design-en.js64-bit- CadCraft
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Bending and compression on the member
The left sides of the two member interaction equations (6.61) and (6.62).
N ÷ (χy N_Rk ÷ γM1) + kyy My ÷ (χLT My,Rk ÷ γM1) + kyz Mz ÷ (Mz,Rk ÷ γM1), and the same with χz, kzy, kzz
Steel member resistance to EN 1993-1-1 frame/frame-design-en.js64-bit- CadCraft
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Equivalent uniform moment factor
The factor Cm of Table B.3 read from a segment's moment diagram.
straight diagram: max(0.6 + 0.4 ψ, 0.4); loaded span: 0.95 + 0.05 αh or 0.90 + 0.10 αh
Steel member resistance to EN 1993-1-1 frame/frame-design-en.js64-bit- CadCraft
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Yield and tensile strength of the steel
The fy and fu used for a member from its grade and thickness.
table value; EN: the lower pair when the thickest part is over 40 mm
Steel member checks on a solved frame frame/frame-design.jsExact- CadCraft
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A diagram value between stations
Reads a force or moment at any distance along the member from the station values.
a = aₖ + (x − xₖ) ÷ (xₖ₊₁ − xₖ) × (aₖ₊₁ − aₖ)
Steel member checks on a solved frame frame/frame-design.js64-bit- CadCraft
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The diagram on one unbraced segment
The stations inside a segment plus interpolated values at its two ends.
Steel member checks on a solved frame frame/frame-design.js64-bit- CadCraft
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Quarter-point moments of a segment
The largest moment of a segment and the moments at its quarter, middle and three-quarter points.
|M| at x₀ + 0.25 L, 0.5 L, 0.75 L; max |M| over the stations
Steel member checks on a solved frame frame/frame-design.js64-bit- CadCraft
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Buckling lengths and segments of a member
The unbraced length, the number of segments and the effective lengths used in the checks.
lb = min(L, override or ratio × L); segments = ⌈L ÷ lb − 1e-9⌉; Lcy = ky L; Lcz = kz lb; Lt = lb
Steel member checks on a solved frame frame/frame-design.js64-bit- CadCraft
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Demands and ratios, AISC 360
Collects each check's demand, capacity and ratio for one member and combination.
ratio = demand ÷ capacity; demand = largest station value
Steel member checks on a solved frame frame/frame-design.js64-bit- CadCraft
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Demands and ratios, EN 1993
Collects each check's demand, resistance and ratio for one member and combination.
ratio = demand ÷ resistance; demand = largest station value
Steel member checks on a solved frame frame/frame-design.js64-bit- CadCraft
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Elastic moduli used in the checks
Chooses E and G for the capacity formulas.
EN: E = 210 000, G = 81 000 MPa; AISC: the model's steel
Steel member checks on a solved frame frame/frame-design.js64-bit- CadCraft
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Deflection against the span limit
The largest deflection off the chord over the service combinations, against L ÷ n.
ratio = deflection ÷ (L ÷ limit)
Steel member checks on a solved frame frame/frame-design.js64-bit- CadCraft
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A combination with its loads scaled
Makes a copy of the model whose governing combination has every factor multiplied by a load factor.
f′ = f × λ
Steel member checks on a solved frame frame/frame-breakit.js64-bit- CadCraft
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Load factor at first failure
The factor on the governing combination at which the first member reaches a utilization of 1.
largest utilization(λ) = 1, found by solving the frame again for each λ
Steel member checks on a solved frame frame/frame-breakit.js64-bit- CadCraft
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Connection utilization
The shear and axial force at a member end against the resistance the app states for the joint.
V = √(Vy² + Vz²); utilization = max(V ÷ shear, |N| ÷ axial)
Steel member checks on a solved frame frame/frame-breakit.js64-bit- CadCraft
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Shear factor and Gauss points
The shear correction factor and the position of the integration points.
k = 5 ÷ 6; ξ, η = ±1 ÷ √3
Plate element for slabs and walls frame/plate.js64-bit- CadCraft
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Jacobian of the element
The map between the element's own square coordinates and the plate's plane, its determinant and inverse.
det J = x,ξ y,η − y,ξ x,η; J⁻¹ = adj(J) ÷ det J
Plate element for slabs and walls frame/plate.js64-bit- CadCraft
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Plate axes, warp and area
The plate's own x, y and normal, its corners in that plane, how far the corners leave the plane, and its area.
n = unit(d₁ × d₂) of the diagonals; warp = max |z| of the corners from the mean plane; area = ½ |Σ (xᵢ yᵢ₊₁ − xᵢ₊₁ yᵢ)|
Plate element for slabs and walls frame/plate.js64-bit- CadCraft
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Plane-stress material matrix
The matrix that turns strains into forces per length, or curvatures into moments per length.
D = f ÷ (1 − ν²) × [[1, ν, 0], [ν, 1, 0], [0, 0, (1 − ν) ÷ 2]]
Plate element for slabs and walls frame/plate.js64-bit- CadCraft
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Element stiffness
The 24 × 24 stiffness of one plate in its own axes and in the model's.
K = ∫ Bᵀ D B dA by 2 × 2 Gauss; D_b = E t³ ÷ (12 (1 − ν²)); D_s = 5⁄6 G t; membrane: k_cc − k_ci k_ii⁻¹ k_ic
Plate element for slabs and walls frame/plate.js64-bit- CadCraft
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Transverse shear at the tying points
The shear strain rows at the four edge midpoints that the element interpolates from.
γ̃_ξ at (0, ∓1); γ̃_η at (∓1, 0)
Plate element for slabs and walls frame/plate.js64-bit- CadCraft
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Shear strains at a point
The two transverse shear strains at an integration point from the tied values.
[γ_x, γ_y] = J⁻¹ [γ̃_ξ, γ̃_η]; γ̃ interpolated linearly between opposite edges
Plate element for slabs and walls frame/plate.js64-bit- CadCraft
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4 × 4 inverse
Inverts the stiffness block of the incompatible modes.
Gauss–Jordan with partial pivoting
Plate element for slabs and walls frame/plate.js64-bit- CadCraft
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Element stiffness in global axes
Turns the plate's stiffness from its own axes to the model's.
K_g = Tᵀ K T, by 3 × 3 blocks
Plate element for slabs and walls frame/plate.js64-bit- CadCraft
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Forces and moments in a plate
Membrane forces, bending and twisting moments and transverse shears per unit length at a point of a plate.
N = D_m ε; M = −D_b κ; Q = D_s γ
Plate element for slabs and walls frame/plate.js64-bit- CadCraft
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Gauss point values to the corners
Corner values of a result from its four integration point values.
bilinear through the 2 × 2 points, read at ξ, η = ±√3
Plate element for slabs and walls frame/plate.js64-bit- CadCraft
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Corner shares of a plate's area
The part of a uniform pressure or of the plate's weight that goes to each corner.
∫ Nᵢ dA by 2 × 2 Gauss
Plate element for slabs and walls frame/plate.js64-bit- CadCraft
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Poisson's ratio of a plate's material
The ratio the plate element uses, from the material's two moduli.
ν = E ÷ (2G) − 1
Frame analysis with slabs, walls and rigid floors frame/plate-solve.js64-bit- CadCraft
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Master point of a rigid floor
The point a floor's in-plan movement is measured at, and each node's offset from it.
x_m = mean of the nodes' x; y_m = mean of the nodes' y (or the point given)
Frame analysis with slabs, walls and rigid floors frame/plate-solve.js64-bit- CadCraft
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Rigid floor constraint
Ties a floor node's two in-plan movements and its rotation about the vertical to the floor's master point.
u_x = U_x − (y − y_m) R_z; u_y = U_y + (x − x_m) R_z; r_z = R_z
Frame analysis with slabs, walls and rigid floors frame/plate-solve.js64-bit- CadCraft
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Skyline Cholesky factorization
Factorizes the stiffness of the whole model once for every load set.
K = L Lᵀ; L_ii = √(K_ii − Σ L_ik²)
Frame analysis with slabs, walls and rigid floors frame/plate-solve.js64-bit- CadCraft
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Forward and back substitution
Solves the factorized system for one load vector.
L y = f; Lᵀ x = y
Frame analysis with slabs, walls and rigid floors frame/plate-solve.js64-bit- CadCraft
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Loads on plates
Turns a plate's own weight and area loads into forces at its corners.
corner force = (∫ Nᵢ dA) × p; own weight p = −factor × f × ρ × 1e-9 × g × t
Frame analysis with slabs, walls and rigid floors frame/plate-solve.js64-bit- CadCraft
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Node displacements from the solution
Gives every node its six displacements, including those tied to a floor's master point.
u_q = Σ c × x_e over the constraint map of q
Frame analysis with slabs, walls and rigid floors frame/plate-solve.js64-bit- CadCraft
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Plate forces into the reactions
Adds each plate's corner forces to the support reactions and stores the plate's center results.
f = K_g u, added at the corners; center results at ξ = η = 0
Frame analysis with slabs, walls and rigid floors frame/plate-solve.js64-bit- CadCraft
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Plate results at the nodes
The moments and forces shown at each node of a slab or wall.
inside: mean of the corner values of the plates at the node; on an edge: a + b x + c y fitted through nearby Gauss values, read at the node
Frame analysis with slabs, walls and rigid floors frame/plate-solve.js64-bit- CadCraft
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Least-squares plane through Gauss values
The value at a node on a slab's edge, from a plane fitted through the integration point values around it.
normal equations 3 × 3, first unknown by Cramer's rule
Frame analysis with slabs, walls and rigid floors frame/plate-solve.js64-bit- CadCraft
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Story drift
How far each rigid floor moves relative to the floor below, at its center and at its worst node.
drift = move(floor) − move(floor below) at the same point; ratio = |drift| ÷ story height
Frame analysis with slabs, walls and rigid floors frame/plate-solve.js64-bit- CadCraft
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Combined plate results
Adds plate results and floor movements of several load sets, each times its factor.
result = Σ fᵢ × resultᵢ
Frame analysis with slabs, walls and rigid floors frame/plate-solve.js64-bit- CadCraft
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Cleaning an outline
Removes repeated points and corners that lie on a straight run, and makes the outline counter-clockwise.
drop a point when |p − q| ≤ 1e-6; drop a corner when |cross| ≤ 1e-9 × |b − a|²
Meshing a slab or wall into plates frame/plate-mesh.js64-bit- CadCraft
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Is the outline square-cornered
Finds the turn that makes every edge of the outline and its openings run along one of two square directions.
turn = atan2 of the longest edge; each edge: min(|dx|, |dy|) ≤ 1e-6 × max(1, length)
Meshing a slab or wall into plates frame/plate-mesh.js64-bit- CadCraft
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Grid mesh
Lays grid lines through every corner and given point and divides each gap into equal parts no longer than the size asked for.
n = ⌈gap ÷ size − 1e-9⌉; line_j = a + (b − a) × j ÷ n
Meshing a slab or wall into plates frame/plate-mesh.js64-bit- CadCraft
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Point inside a polygon
Decides whether a grid cell's center lies inside the outline or inside an opening.
even–odd crossing count
Meshing a slab or wall into plates frame/plate-mesh.js64-bit- CadCraft
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Mesh of a four-corner outline
A structured mesh between the opposite edges of a convex four-corner outline.
P(s, t) = (1 − s)(1 − t) P₀ + s (1 − t) P₁ + s t P₂ + (1 − s) t P₃; s = i ÷ n, t = j ÷ m
Meshing a slab or wall into plates frame/plate-mesh.js64-bit- CadCraft
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A calculation is added only after its source was read. Each statement can be checked in the code shown on its policy's page; the app repositories are public. When a release changes a calculation, its page says so until it has been read again.