The amount of test cycles required to find out the fatigue stress of hard aluminium alloys is ____________(a) 64,000,900,000(b) 500,000,000(c) 3000(d) 27I have been asked this question during a job interview.The doubt is from Aircraft Materials in chapter Testing Aircraft Materials of Aerospace Materials & Processes

The amount of test cycles required to find out the fatigue stress of h

1.	The amount of test cycles required to find out the fatigue stress of hard aluminium alloys is ____________(a) 64,000,900,000(b) 500,000,000(c) 3000(d) 27I have been asked this question during a job interview.The doubt is from Aircraft Materials in chapter Testing Aircraft Materials of Aerospace Materials & Processes
Answer» Correct OPTION is (b) 500,000,000 To elaborate: A HUGE number of test CYCLES are REQUIRED to determine the fatigue strength of a material. The number of cycles required for aluminium alloys is 500,000,000. It is the same for MAGNESIUM alloys as well.

Discussion

No Comment Found

Related InterviewSolutions

In case of shore scleroscope hardness, the number considered is the average of __________ determinations.(a) 5(b) 26(c) 1(d) 333I got this question in an online quiz.I'm obligated to ask this question of Aircraft Materials in chapter Testing Aircraft Materials of Aerospace Materials & Processes
If the expected yield strength of a material is 50,000 pounds per square inch and modulus of elasticity is 10,000, what is the normal elongation of the material?(a) 50,000,000 inch per inch gage length(b) 5 inch per inch gage length(c) 50 inch per inch gage length(d) 5 inch per inch gage lengthThe question was asked by my school principal while I was bunking the class.My doubt stems from Aircraft Materials in portion Testing Aircraft Materials of Aerospace Materials & Processes
What is the diameter of a typical specimen used in fatigue testing?(a) 2000 inches(b) 0.0005 inches(c) 1 inch(d) 26 inchesI have been asked this question in homework.This interesting question is from Aircraft Materials topic in division Testing Aircraft Materials of Aerospace Materials & Processes
It is usually very easy to obtain the exact bending radius desired in a bending test.(a) True(b) FalseThis question was addressed to me in a job interview.My query is from Aircraft Materials topic in section Testing Aircraft Materials of Aerospace Materials & Processes
On _________ materials, impact test cannot be conducted.(a) steel(b) solid(c) room temperature(d) extremely ductileI got this question in unit test.The question is from Impact Test topic in portion Testing Aircraft Materials of Aerospace Materials & Processes
How far must the specimen be withdrawn with respect to the coil in demagnetization?(a) 00.7 inches(b) 26 inches(c) 18 inches(d) 4 inchesI had been asked this question during an interview.I would like to ask this question from Testing Aircraft Materials topic in section Testing Aircraft Materials of Aerospace Materials & Processes
One of the disadvantages of radiography is that it is ___________(a) destructive(b) faster(c) temporary record(d) time-consumingI have been asked this question in a job interview.I would like to ask this question from Testing Aircraft Materials topic in chapter Testing Aircraft Materials of Aerospace Materials & Processes
During tension testing, the material must be held in _____________ alignment.(a) normal(b) axial(c) parallel(d) diabolicalI had been asked this question by my college professor while I was bunking the class.The question is from Aircraft Materials topic in section Testing Aircraft Materials of Aerospace Materials & Processes
The tension testing machine (crosshead) should not cross a speed of ___________ inch per inch of the gage length per minute until the yield point.(a) 1/11(b) 2(c) 1/16(d) 2/5The question was asked in a job interview.The doubt is from Aircraft Materials in chapter Testing Aircraft Materials of Aerospace Materials & Processes
The proof stress of a material of 3 inches gage length is the highest stress it can withstand without a permanent set of above ___________ inch.(a) 0.0003(b) 0.21(c) 0.05(d) 0.004I had been asked this question in an interview.Question is taken from Aircraft Materials topic in section Testing Aircraft Materials of Aerospace Materials & Processes

Discussion

No Comment Found

Related InterviewSolutions

Reply to Comment