Machine-translated by Google. Questions are authored in English.
Top

Fatigue and Damage Tolerance Questions and Answers

Answer: C

The philosophy accepts cracking as inevitable and builds the inspection programme into the design itself. Crack growth analysis and inspection interval are inseparable, which is why damage tolerance is a design discipline rather than a maintenance one.

Please log in or register to report this question.

Answer: D

Static strength answers the first of the alternatives; fatigue and damage tolerance answer the question of endurance over tens of thousands of flights. The two together, and only together, establish that a structure is fit for service.

Please log in or register to report this question.

Answer: A

Correct answer: Extract discrete countable cycles

A real load history is an irregular sequence of peaks and troughs with no obvious cycles in it, and Miner’s rule needs discrete cycles of known amplitude and mean. Rainflow counting pairs the reversals in a way that matches the material’s hysteresis behaviour, so that a nested small excursion is counted as its own cycle within the larger one containing it.

Please log in or register to report this question.

Answer: B

A single test article cannot represent the whole fleet, and no spectrum exactly matches how every operator flies. Factors of three or more on life are common, and the demonstrated life must therefore be several times the certified one.

Please log in or register to report this question.

Answer: C

Correct answer: Eddy current, ultrasonic and penetrant

These three are the mainstays for airframe crack detection, and each has its place: eddy current for surface and near-surface cracks including those under a fastener head, ultrasonic for buried defects and thickness, penetrant for surface-breaking cracks in non-ferrous parts. The other options all destroy or overload the part, which defeats the purpose.

Please log in or register to report this question.

96.

A load history yields \( 500 \) cycles at a level with a life of \( 10^5 \) and \( 2000 \) at a level with a life of \( 10^4 \). The Miner sum is

Answer: D

Correct answer: 0.205

\[ \frac{500}{10^5} + \frac{2000}{10^4} = 0.005 + 0.200 = 0.205. \] The higher level dominates completely: four times as many cycles at a life ten times shorter contributes forty times the damage. This is characteristic of fatigue spectra, where a small number of severe cycles accounts for most of the life consumed.

Please log in or register to report this question.

97.

Assertion (A): A rainflow count is a necessary preliminary to applying Miner's rule.

Reason (R): Miner's rule requires discrete cycles of known amplitude and mean.

Select the correct answer from the options below.

Answer: A

Correct answer: Both A and R are true, and R is the correct explanation of A

Both are true and the reason gives the mechanism. Miner’s rule works on discrete cycles of known amplitude and mean, taking \( n_i/N_i \) at each level, and a measured load history contains no such cycles until they have been extracted. Rainflow counting performs that extraction, so it is the necessary step between the strain record and the damage sum.

Please log in or register to report this question.

98.

Consider the following statements about inspection methods:

1. Each method has a characteristic detectable crack size.

2. That size feeds directly into the inspection interval calculation.

3. All methods detect the same minimum crack size.

Which of the statements given above is or are correct?

Answer: B

The first two are correct. The third is false and is the reason method selection matters: eddy current and ultrasonic inspection find far smaller cracks than a visual check, and that difference translates directly into maintenance interval.

Please log in or register to report this question.

Answer: C

Static strength is demonstrated separately and has its own factors. The scatter factor addresses the variability inherent in fatigue itself, where nominally identical specimens can differ in life by an order of magnitude.

Please log in or register to report this question.

Answer: D

The inspection intervals are part of the safety case, not a maintenance convenience, and deferring them removes the mechanism by which cracks are caught. Usage significantly harsher than assumed also warrants a shorter interval than the baseline.

Please log in or register to report this question.

Loading…
Tags: Fatigue and Damage Tolerance Questions and Answers || Fatigue and Damage Tolerance MCQ Questions and Answers || Fatigue and Damage Tolerance GK Questions and Answers || Fatigue and Damage Tolerance GK MCQ Questions || Fatigue and Damage Tolerance Multiple Choice Questions and Answers || Fatigue and Damage Tolerance GK || GK on Fatigue and Damage Tolerance || Aerospace Structures Questions and Answers || Aerospace Structures MCQ Questions and Answers || Aerospace Structures GK Questions and Answers || GK on Aerospace Structures