ASME B106.1M Sizing & Standard Stock Recommendation

Iterative multiaxial fatigue sizing with Marin modification factors and Langer first-cycle yield verification.

Minimum Required Outer (D_o)
31.094mm
Target FOS = 2.00 (ASME-ELLIPTIC)
Recommended Stock Size
32.000mm
Standard Commercial Bar
Reserve Fatigue FOS (n_f)
2.09
Infinite Life S_e Criterion
Langer Static Yield FOS (n_y)
2.09
Yield Guard: σ_a' + σ_m' ≤ S_y

Haigh Stress Diagram & Fatigue Envelope

Alternating stress (σ_a') vs Mean stress (σ_m') superimposed against ASME, Goodman, Soderberg, and Langer yield boundaries.

PASS (n_f = 1.92)
Mean von Mises Stress σ_m' (MPa)Alternating Stress σ_a' (MPa)Point (94, 68)Sy=310Sut=585Se=170
ASME Elliptic
Goodman
Soderberg
Gerber
Langer Yield

Fatigue Failure Criteria Comparison Matrix

Comparative sizing envelopes and reserve safety factors across ASME B106.1M, Goodman, Soderberg, and Gerber models.

Failure CriterionGoverning EquationReq. DiameterFatigue FOS (n_f)Status
DE-ASME EllipticActive

Elliptic curve bounded by Se and Sy. Most realistic for ductile steels under fluctuating torsion & bending.

(\sigma_a' / S_e)^2 + (\sigma_m' / S_y)^2 = 1/n^231.094 mm2.00SAFE
DE-Goodman

Linear boundary from Se to Sut. Standard practice for brittle components and conservative machine design.

\sigma_a' / S_e + \sigma_m' / S_{ut} = 1/n32.289 mm1.79SAFE
DE-Soderberg

Linear boundary from Se to Sy. Ensures complete protection against first-cycle yielding without extra check.

\sigma_a' / S_e + \sigma_m' / S_y = 1/n34.877 mm1.43SAFE
DE-Gerber

Parabolic curve from Se to Sut. Best statistical fit for pure ductile laboratory test specimens.

n \sigma_a' / S_e + (n \sigma_m' / S_{ut})^2 = 130.093 mm2.20SAFE
Langer Static Yield

Checks maximum combined von Mises stress (σ_a' + σ_m' ≤ Sy / n_y) to prevent localized plastic deformation.

\sigma_a' + \sigma_m' = S_y / n_y31.533 mm1.92SAFE

Torsional Rigidity & Whirling Critical Speed

Elastic angular twist compliance and Rayleigh-Ritz fundamental rotational resonance exclusion zone (±20% Nc).

SAFE REGION
Torsional Angular Twist (θ)EXCEEDED
Total Twist Angle1.260° (0.0220 rad)
Specific Twist Rate1.575 deg/m
Allowable Limit≤ 1.00 deg/m
Min Req. Diameter for Twist34.831 mm
Rayleigh-Ritz Critical Speed (N_c)Ratio: 0.0%
Fundamental Critical Speed5850 RPM
Operating Speed0 RPM
±20% Resonance Exclusion Zone4680 – 7020 RPM

Marin Endurance Modification Factor Breakdown

Iterative derivation of fully corrected shaft fatigue endurance limit: S_e = k_a · k_b · k_c · k_d · k_e · S_e'

Corrected Endurance S_e170.3 MPa
k_a
0.833
Surface Finish Factor
Condition: machined
k_b
0.858
Size Modification Factor
Converged diameter size effect
k_c
0.814
Reliability Factor
Reliability: 99.00%
k_d
1.000
Temperature Factor
Operating temp: 20°
k_e
1.000
Miscellaneous Factor
Stress concentration & duty cycle
S_e =(0.582)×292.5 MPa=170.3 MPa
Base endurance limit S_e' = 0.50 S_ut

Calculation Summary

Input Parameters
Shaft ProfileSolid Bar
Steel MaterialAISI-1045
Tensile Strength (S_ut)585MPa
Yield Strength (S_y)310MPa
Fatigue Failure ModelASME-ELLIPTIC
Geometric Notchprofile-keyway
Alternating Bending (M_a)100N·m
Mean Torque (T_m)200N·m
Design FOS (n_d)2
Shaft Span (L)800mm
Calculated Results
Min Required Outer Diameter (D_o)31.094mm
KEY
Recommended Stock Bar Size32.000mm
Reserve Fatigue FOS (n_f)1.92
Langer Static Yield FOS (n_y)1.92
Safety Notes
Torsional Twist Limit Exceeded: Specific angular deflection (1.57 deg/m) exceeds allowable (1 deg/m).

Mathematical Models & Equations

ASME B106.1M Multiaxial Fatigue Governing Sizing Equation
d = \left[ \frac{16 \cdot n}{\pi} \sqrt{ \left( \frac{A}{S_e} \right)^2 + \left( \frac{B}{S_y} \right)^2 } \right]^{1/3} \quad \text{where } A = \sqrt{4(k_b M_a)^2 + 3(k_t T_a)^2}, \; B = \sqrt{4(k_b M_m)^2 + 3(k_t T_m)^2}

Verification Calculation Log

  • 1Applied Nominal Torque: T = 200.00\text{ N·m} (Mean T_m = 200.00\text{ N·m}, Alternating T_a = 0.00\text{ N·m})
    • •Bending Moment Components: Alternating M_a = 100.00\text{ N·m}, Mean M_m = 0.00\text{ N·m} (Stress concentrations: k_b = 2.00, k_t = 1.60 for profile-keyway)
    • •Material Properties: S_{ut} = 585.0\text{ MPa}, S_y = 310.0\text{ MPa}, S_e' = 0.5 S_{ut} = 292.5\text{ MPa}
    • •Marin Fatigue Modification: S_e = k_a k_b k_c k_d k_e S_e' = (0.833)(0.858)(0.814)(1.000)(1.00)(292.5) = 170.3\text{ MPa}
    • •Solve Required Solid Shaft Diameter (DE-ASME Elliptic, n = 2): d = 31.094\text{ mm}
    • •Recommended Standard Stock Size: 32.000\text{ mm} (Standard stock safety factor n_f = 2.09, Static yield factor n_y = 2.09)
    • •Torsional Rigidity Check (L = 800\text{ mm}): \theta = \frac{T L}{G J} = 1.260^\circ \rightarrow 1.575\text{ deg/m} (Limit: 1.00\text{ deg/m} - FAIL)
    • •Rayleigh-Ritz Critical Speed: Fundamental Whirling Speed N_c = 5850\text{ rpm}, Operating Speed = 0\text{ rpm} (SAFE)

Shaft Fatigue Engineering Rules & Guidelines

Engineering Application Notes

ASME B106.1M & Shigley Shaft Design Guidelines: 1. Multiaxial Fatigue Stress States: Rotating shafts undergo fully reversed bending stress (σ_a) and steady or pulsating torsional shear (τ_m). Always use ASME Elliptic or DE-Goodman criteria for sizing. 2. Stress Concentration Mitigation: Generous fillet radii (r/d ≥ 0.10) at bearing and gear shoulders reduce stress concentration factors (Kf) by over 30%, drastically extending fatigue life. 3. Keyway Corrections: Profile end-milled keyways cut through the highest stress fibers. Standard ASME practice applies Kf = 2.0 and Kfs = 1.6 to alternating and mean load components. 4. Rayleigh-Ritz Critical Speed Exclusion: Ensure machine operating speed is kept outside the ±20% resonance envelope (0.80 Nc to 1.20 Nc) to avoid catastrophic whirling failure. 5. Angular Torsional Compliance: For precision machine tool drives, keep torsional twist below 0.25°/m (0.08°/ft) to prevent servo oscillation and gear transmission chatter.