22-Mec-B9 Advanced Engineering Structures · December 2017
Question 3 of 8: Coffin–Manson constants and Miner cumulative damage
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Exams, December 2017 — 16-Mec-B9
Advanced Engineering Structures. Three hours, open book, any non-communicating
calculator permitted. The paper prints eight questions of equal value (20 marks each) and
states that any five constitute a complete exam paper. All eight are solved below,
because the set is a study resource rather than a sitting.
Reference texts.
T. H. G. Megson, Aircraft Structures for Engineering Students, 6th ed. —
unsymmetrical bending, shear flow in open and closed thin-walled sections, shear centre,
structural idealisation, single- and multi-cell torsion (Ch. 15, 16, 17, 20, 23).
A. C. Ugural and S. K. Fenster, Advanced Strength and Applied Elasticity, 5th ed.
— three-dimensional states of stress, principal stresses, the Tresca and von Mises yield
criteria (Ch. 1, 4).
A. P. Boresi and R. J. Schmidt, Advanced Mechanics of Materials, 6th ed. —
shear centre, torsion of multiply connected cells, column stability (Ch. 6, 12).
N. E. Dowling, Mechanical Behavior of Materials, 4th ed. — strain-life
fatigue, the Coffin–Manson relation, the Palmgren–Miner rule and Paris-law crack
growth (Ch. 9, 11, 14).
R. C. Hibbeler, Mechanics of Materials, 10th ed. — Euler buckling of
pin-ended columns, slenderness ratio and the transition slenderness (Ch. 13).
Sign convention used throughout. A single right-handed frame is used
for every thin-walled question: x runs along the span from the root to the free end,
Y is vertically upward and Z horizontally to the right, both measured from the
section centroid. Direct stress is written $\sigma_x = aZ + bY$, and the two coefficients follow
from $aI_{ZZ} + bI_{YZ} = M_Y$ and $aI_{YZ} + bI_{YY} = M_Z$, in which
$I_{ZZ}=\int Z^{2}\,dA$, $I_{YY}=\int Y^{2}\,dA$, $I_{YZ}=\int ZY\,dA$,
$M_Y \equiv \int \sigma_x Z\,dA$ and $M_Z \equiv \int \sigma_x Y\,dA$. This one pair of
equations replaces the memorised unsymmetrical-bending fraction and is self-checking: for a
cantilever carrying a tip load, the fibres on the side the load points toward must go into
compression.
Question 3: Coffin–Manson constants and Miner cumulative damage (20 marks)
Given. Four constant-amplitude low-cycle fatigue tests on one
alloy, followed by a three-block service history applied to a component made from it.
Given data — strain-cycling test results
Range of plastic strain $\Delta\varepsilon$
Cycles to failure $N$
0.0360
260
0.0211
990
0.0120
2700
0.0070
15 500
Service history: 390 cycles at $\Delta\varepsilon = 0.019$, then 100 cycles at
$\Delta\varepsilon = 0.025$, then the balance of the life at $\Delta\varepsilon = 0.010$.
Find. (a) the best-fit constants $C$ and $\alpha$ in
$\Delta\varepsilon = CN^{\alpha}$; (b) the total number of cycles the component survives under
the three-block history, using the linear Palmgren–Miner damage rule.
The four test points and the least-squares Coffin–Manson line. A power law
plots as a straight line on logarithmic axes, so fitting it is an ordinary linear regression of
$\ln \Delta\varepsilon$ on $\ln N$.
Approach. Linearise the power law by taking logarithms, fit by least squares
to obtain $\alpha$ and $C$, invert the fitted law to get an allowable life at each of the three
service strain ranges, and close the Miner sum at unity to solve for the unknown third block.
Part (a) — linearise the power law. Taking natural logarithms of
$\Delta\varepsilon = CN^{\alpha}$ gives
$\ln\Delta\varepsilon = \ln C + \alpha \ln N$, a straight line of slope $\alpha$ and intercept
$\ln C$ in the transformed variables $x = \ln N$, $y = \ln\Delta\varepsilon$.
Fit the line by least squares. With the four transformed points, the normal
equations give
$$\alpha = \frac{n\sum xy-\sum x\sum y}{n\sum x^{2}-(\sum x)^{2}} = -0.4079, \qquad
\ln C = \frac{\sum y - \alpha \sum x}{n} = -1.0819 .$$
Exponentiating the intercept,
$$\boxed{\Delta\varepsilon = 0.3390\,N^{-0.4079}}$$
with a coefficient of determination $R^{2} = 0.987$, confirming that a single power law
represents all four decades of the data well.
Sanity-check the exponent. A Coffin–Manson exponent near $-0.4$ to
$-0.6$ is the expected range for structural metals, and the fitted $-0.408$ sits comfortably
inside it, so neither a transcription error nor a units slip has crept into the data.
Part (b) — invert the law to get allowable lives. Rearranging,
$N = \left(\Delta\varepsilon / C\right)^{1/\alpha}$, so for the three service blocks
$$N_1 = 1169\ \text{cycles at } 0.019, \qquad N_2 = 597\ \text{cycles at } 0.025, \qquad
N_3 = 5641\ \text{cycles at } 0.010 .$$
The larger strain range gives the shorter life, as it must.
Accumulate the damage from the two completed blocks. Miner's rule adds the
fractional lives consumed:
$$D_{1,2} = \frac{n_1}{N_1}+\frac{n_2}{N_2} = \frac{390}{1169}+\frac{100}{597}
= 0.3335 + 0.1676 = 0.5011 .$$
Just over half the fatigue life is used up in the first 490 cycles.
Solve for the third block. Failure occurs when the total damage reaches
unity, so the number of further cycles the component tolerates at
$\Delta\varepsilon = 0.010$ is
$$n_3 = \left(1 - D_{1,2}\right) N_3 = 0.4989 \times 5641 = 2815\ \text{cycles}.$$
Add the blocks for the total life.
$$\boxed{N_{\text{total}} = 390 + 100 + 2815 = 3305 \ \text{cycles}}$$
Rounding to the precision the data justify, the component survives approximately
$3.3\times10^{3}$ cycles.
Verify the damage closes on unity. Re-evaluating
$390/1169 + 100/597 + 2815/5641$ returns $1.0000$ to ten decimal places, which is the arithmetic
check that the third block was solved rather than assumed.