EngivonMechanical
Discipline Hub20 Verified Calculators

Mechanical Engineering Calculators

Precision calculation engines and interactive engineering tools for machine design, power transmission, rotordynamics, fatigue verification, and workshop manufacturing. Built on peer-reviewed mechanics and international engineering standards.

Calculate bearing L10 rating life per ISO 281 in million revolutions and operating hours with Weibull reliability and equivalent dynamic load adjustments.

Core FormulaL₁₀ = (C / P)ᵖ (p = 3 for ball, 10/3 for roller)
Fatigue LifeISO 281Weibull ReliabilityDynamic Load C
ISO 281:2007 +2Launch Tool

Calculate geometric resultant force (F = √(Fr² + Fa²)), ISO 281 dynamic equivalent load (P = X·V·Fr + Y·Fa), and ISO 76 static equivalent load (P₀).

Core FormulaF = √(Fr² + Fa²) • P = X·V·Fr + Y·Fa • P₀ = max(X₀·Fr + Y₀·Fa, Fr)
Machine DesignISO 281Equivalent LoadISO 76 Static
ISO 281:2007 +2Launch Tool

Determine belt pitch length, wrap angles, and center distance for open and crossed belt drives with standard V-belt matching and motor slot tension allowances.

Core FormulaL = 2C + (π/2)(D + d) + (D − d)² / (4C)
Power TransmissionV-Belt & TimingOpen & CrossedWrap Angles
ISO 4184 +3Launch Tool

Calculate effective belt tension (Fe = P/v = 2T/D), tight-side (T1) and slack-side (T2) dynamic tensions, centrifugal liftoff (Fc = m'v²), and shaft bearing loads.

Core FormulaFe = P/v = 2T/D • (T₁ − Fc)/(T₂ − Fc) = e^(μθ)
Power TransmissionEuler-EytelweinCentrifugal TensionBearing Loads
ISO 4184 +3Launch Tool

Determine standard parallel key size, shaft keyway depth (t₁), hub keyway depth (t₂), and caliper inspection depth from shaft diameter with ISO tolerance fits.

Core Formulad − t₁ Caliper Check & (t₁ + t₂ > h) Radial Clearance
Machine ElementsDIN 6885-1ANSI B17.1ISO 773 Fits
DIN 6885-1 +2Launch Tool

Calculate lifting and lowering torque, drive efficiency, thrust capacity, and self-locking conditions for square, Acme, and trapezoidal power screws.

Core FormulaT_R = (F·d_m/2) · [(l + π·μ·d_m·sec α) / (π·d_m − μ·l·sec α)] + T_c
Linear MotionAcme & TrapezoidalDrive EfficiencySelf-Locking
ISO 2904 +2Launch Tool

Estimate the fundamental lateral critical speed (first natural frequency) and resonance avoidance safety margins for simply supported and fixed rotating shafts.

Core Formulaω_n = π² · √(E·I / (m·L⁴)) (Dunkerley & Rayleigh-Ritz)
RotordynamicsVibration AnalysisNatural FrequencyResonance
ISO 10816 +2Launch Tool

Compute shear stress for direct single/double shear in joints, linear torsional stress in solid and hollow circular shafts, and transverse Jourawski beam shear.

Core Formulaτ = F/A (Direct) • τ = T·c/J (Torsion) • τ_max = 1.5·V/A (Beam)
Mechanics of MaterialsDirect & Double ShearShaft TorsionJourawski
ASTM E8/E8M +2Launch Tool

Determine exact tap drill sizes and theoretical thread engagement percentages for ISO Metric and Unified (UNC/UNF) threads across cutting and roll forming taps.

Core FormulaTDS = Major Dia − (% Engagement / 100) · 1.29904 · Pitch
Machining & CNCISO Metric (M)Unified (UNC/UNF)Roll Forming
ISO 68-1 +3Launch Tool

Calculate driven RPM from pulley diameters, find required pulley size for a target speed, determine speed ratio, and compute belt linear velocity.

Core FormulaD₁N₁ = D₂N₂ • v = πDN / 60
Power TransmissionBelt DriveSpeed RatioRPM
Shigley Ch. 17 +1Launch Tool

Calculate belt linear velocity (v), required motor RPM, and sheave pitch diameter with slip factor and bending fatigue cycles.

Core Formulav = π·D·N / 60 • N = 60v / (π·D)
Power TransmissionPitch Line VelocitySlip OffsetFlex Fatigue
ISO 5296 +3Launch Tool

Determine roller chain link count (even pitches) and exact shaft center distance per ASME B29.1 and ISO 606 standards.

Core FormulaL = 2C + (N₁+N₂)/2 + (N₂−N₁)²/(4π²C)
Power TransmissionRoller ChainASME B29.1ISO 606
ASME B29.1 +3Launch Tool

Calculate sprocket pitch diameter (P.D.), outer/root circles, chordal action velocity ripple, and drive reduction ratios.

Core FormulaP.D. = p / sin(180°/N) • O.D. = p·[0.6 + cot(180°/N)]
Power TransmissionPitch DiameterChordal ActionSpeed Ratio
ASME B29.1 +3Launch Tool

Calculate torsional shear stress for solid and hollow circular shafts (τ = Tr/J), or determine the minimum shaft diameter for an allowable stress limit.

Core Formulaτ = 16T/(πd³) • d = [16T/(πτ)]^(1/3)
Shaft DesignTorsional ShearPolar MomentReverse Sizing
Shigley Ch. 3 & 7 +2Launch Tool

Calculate the angle of twist (θ = TL/GJ) for solid and hollow shafts with material presets for shear modulus, twist rate analysis, and reverse diameter sizing.

Core Formulaθ = TL/(GJ) • d = [32TL/(πGθ)]^(1/4)
Torsional DeformationTwist RateShear ModulusStiffness
Shigley Ch. 3 +2Launch Tool

Calculate bending stress (σ = Mc/I) for rectangular, circular, hollow circular, I-section, and custom cross-sections with section modulus output.

Core Formulaσ = Mc/I = M/S • S = I/c
Beam DesignFlexure FormulaSection ModulusNeutral Axis
Shigley Ch. 3 +3Launch Tool

Look up clearance hole diameters, nominal drill sizes, and ISO 286 limit tolerances (H12, H13, H14) for M1.6–M100 bolts across Close, Normal, and Loose fits per ASME B18.2.8.

Core FormulaC = Dh − Dn • Cr = C / 2 • ISO 286 (H12/H13/H14)
Fasteners & BoltsASME B18.2.8ISO 286 FitsM1.6 to M100
ASME B18.2.8-1999 (R2017) +2Launch Tool

Look up modulus of elasticity (E), shear modulus (G), bulk modulus (K), and Poisson's ratio (ν) for 24+ carbon, alloy, structural, stainless, and tool steels with Hooke's law and Eurocode 3 fire reduction factors.

Core Formulaσ = E · ε • G = E / [2(1 + ν)] • δ = F·L / (A·E)
Materials & MechanicsModulus of ElasticityHooke's LawEurocode 3
ASTM A36/A572 +4Launch Tool

Calculate mass moments of inertia (Iz, Ix, Iy) for solid and hollow cylinders with center-of-mass principal axes, density-based mass, parallel axis offsets, and rotational kinetic energy.

Core FormulaIz = ½ M r² • Ix = 1/12 M (3r² + h²) • I = I_CM + M d²
Rotational DynamicsRigid Body MechanicsFlywheels & DrumsParallel Axis
Beer & Johnston Ch. 9 +3Launch Tool

Compute elastic deflection, slope, shear force, and bending moment diagrams for simply supported, cantilever, fixed, and propped beams under point and distributed loads.

Core Formulaδ_max = P·L³ / (48·E·I) • δ_max = 5·w·L⁴ / (384·E·I)
Structural MechanicsEuler-BernoulliDeflection & SlopeSFD & BMD
AISC 360 +3Launch Tool

Evidence-Based Engineering Methodology

Every calculator in our mechanical suite is engineered for transparency, scientific accuracy, and auditability. We eliminate “black box” calculations by exposing full step-by-step arithmetic derivations, underlying assumptions, and authoritative standard references.

International Standards

Aligned with ISO, DIN, ANSI/ASME, and AGMA standards to ensure compliance with global manufacturing specifications.

Textbook & Research Proven

Formulated per standard references including Shigley's Mechanical Engineering Design, Beer & Johnston, and Machinery's Handbook.

Unit Correctness & Verification

Comprehensive bidirectional conversion across SI Metric and US Customary imperial units with 280+ automated unit tests.