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FORMULA SHEET: Fatigue, Fracture Mechanics Structural Mechanics σ i = M x y i I xx M y x i I yy + F A ε x = σ x E ν E ( σ y +σ z ) + αΔT Fatigue: Machined Components σ ar m N=Cσ ar , 1 m N 1 =σ ar ,2 m N 2 m= log ( N 2 N 1 ) log ( σ ar , 1 σ ar , 2 ) N R = { ( σ ar ,1 σ ar ) m N 1 0.9 σ u ≥σ ar ≥σ er σ ar <σ er OR σ ar N b =Cσ ar , 1 N 1 b =σ ar ,2 N 2 b b= log ( σ ar , 1 σ ar , 2 ) log ( N 2 N 1 ) N R = { ( σ ar ,1 σ ar ) 1 b N 1 0.9 f ut ≥σ ar ≥S e σ ar < S e Endurance limit estimates (see Dowling Table 10.1) σ erb = { 0.25BHN ksi for BHN ≤ 400 100 ksi forBHN >400 Steel σ erb = { 0.5 σ u for σ u 200 ksi ( 1400 MPa 100 ksi ( 700 MPa) for σ u >200 ksi ( 1400 MPa Cast Iron + Cast Steels: σ erb = { 0.45 σ u for σ u 600 MPa 275 MPa forσ u >600 MPa Stress concentrations K f : σ sc =K t S K t = σ sc S K f = σ erb (unnotched ) σ erb ( nothced ) K f =1+ K t 1 ( 1+ α r ) Approximations for α: α= [ 300 σ u [ ksi ] ] 1.8 × 10 3 . ¿ [ 300 × 6.89 σ u [ MPa ] ] 1.8 × 10 3 × 25.4 mm Peterson for steels (Dowling, 2013, p. 498): log α =2.654 × 10 7 σ u 2 1.309 × 10 3 σ u + 0.01103 α [ ¿ mm ]=10 log α ( 345 ≤σ u 2070 MPa ) ¿ 10 2.654 ×10 7 σ u 2 1.309 × 10 3 σ u +0.01103 Typical values are: α= { 0.51 mm aluminiumalloys 0.25 mm annealednormalizedlow carbo 0.064 mm quenchedtemperedsteel K f ' :

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FORMULA SHEET: Fatigue, Fracture MechanicsStructural Mechanics

Fatigue: Machined Components

OR

Endurance limit estimates (see Dowling Table 10.1)

Steel

Cast Iron + Cast Steels:

Stress concentrations

· :

· Approximations for :

Peterson for steels (Dowling, 2013, p. 498):

Typical values are:

· :

Mean stress correction

Approach

Equations

Modified Goodman

Gerber

Morrow

SWT

Walker

Juvinall & Budynas (Dowling, 2013, p. Table 10.1)

Juvinall

Budynas:

Modifying factors

Size:

Load:

for axial loading if the fatigue S-N curve was obtained from completely reversed bending loading.

Temperature:

Reliability:

Fatigue: Large scale manufactured components

Partial factor for fatigue:

Assessment

Consequence of failure

Low

High

Damage tolerant

1.0

1.15

Safe life

1.15

1.35

Temperature:

0.6

0.4

0.8

Grinding & TIG dressing:

Effective stress range:

Steel:

Aluminium:

Peening:

Effective stress range:

Fracture Mechanics

Universal equation:

Plastic collapse:

Fracture:

Stress concentration factors:

Centre cracked plate:

Single edge crack:

Double edge crack:

LEFM

Fracture toughness estimation:

Lower limit:

Note, in Joule, in

Crack growth

Pressure equipment

Interpolation on a logarithmic scale using your ruler

CONVERSIONS

1 ksi = 6.89 MPa

Detail catgories

Joint efficiencies

Vessels – Dangerous gas

Figure 1: Design categorization of vessels containing dangerous gas

Vessels – Dangerous liquids

Source: (SANS 347, 2012)

Figure 2: Design categorization of vessels containing dangerous liquids

Piping – Dangerous gas

Similar graphs are available for piping of non-dangerous gas, dangerous liquids and non-dangerous liquids.

Source: (SANS 347, 2012, p. 16)

Transportable container and vessels for dangerous gas

Vessels: Non-dangerous gas

Source: (SANS 347, 2012, p. 12)

Figure 3: Design categorization of vessels: non-dangerous gas