Preventing fatigue crack propagation in aircraft

Chapter 6, Problem 14E

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QUESTION:

Preventing fatigue crack propagation in aircraft structures is an important element of aircraft safety. An engineering study to investigate fatigue crack in n = 9 cyclically loaded wing boxes reported the following crack lengths (in mm): 2.13, 2.96, 3.02, 1.82, 1.15, 1.37, 2.04, 2.47, 2.60. Calculate the sample mean and sample standard deviation. Prepare a dot diagram of the data.

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QUESTION:

Preventing fatigue crack propagation in aircraft structures is an important element of aircraft safety. An engineering study to investigate fatigue crack in n = 9 cyclically loaded wing boxes reported the following crack lengths (in mm): 2.13, 2.96, 3.02, 1.82, 1.15, 1.37, 2.04, 2.47, 2.60. Calculate the sample mean and sample standard deviation. Prepare a dot diagram of the data.

ANSWER:

Solution:

Step 1 of 2:

       Given the 9 observations are

       

2.13

2.96

3.02

1.82

1.15

1.37

2.04

2.47

2.60

  We need to calculate the sample mean and sample standard deviation. And to prepare a dot diagram of the data.        


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