InterviewSolution
This section includes InterviewSolutions, each offering curated multiple-choice questions to sharpen your knowledge and support exam preparation. Choose a topic below to get started.
| 1. |
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 |
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Answer» Correct choice is (a) 5 |
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| 2. |
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 |
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Answer» Right ANSWER is (b) 5 inch per inch gage length |
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| 3. |
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 |
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Answer» Right choice is (c) 1 INCH |
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| 4. |
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 |
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Answer» The CORRECT choice is (b) False |
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| 5. |
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 |
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Answer» CORRECT choice is (d) extremely DUCTILE Explanation: The IMPACT test cannot be conducted in the required way on materials that are extremely ductile. This is due to the fact that these types of materials BEND while breaking. The experiment can be conducted in room temperature. |
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| 6. |
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 |
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Answer» The CORRECT option is (c) 18 inches |
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| 7. |
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 |
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Answer» Correct answer is (d) time-consuming |
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| 8. |
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 |
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Answer» Right ANSWER is (a) normal |
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| 9. |
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 |
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Answer» Right choice is (c) 1/16 |
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| 10. |
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 |
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Answer» The correct answer is (a) 0.0003 |
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| 11. |
Tension test can give us the yield strength of a material.(a) True(b) FalseI have been asked this question during an online exam.The above asked question is from Aircraft Materials topic in portion Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The correct answer is (a) True |
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| 12. |
The extension under load method is easier to use in finding yield strength because ___________(a) no necessity to plot a curve(b) it is not easier(c) it is the only method available(d) randomnessThe question was posed to me by my school principal while I was bunking the class.Question is from Aircraft Materials in portion Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The CORRECT ANSWER is (a) no necessity to plot a curve |
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| 13. |
The flattening test while being used for bronze tubing must consider the thickness of the tube to be not more than ____ times wall thickness.(a) 3(b) 2(c) 4(d) 1The question was asked in semester exam.This question is from Aircraft Materials in division Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The CORRECT choice is (a) 3 |
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| 14. |
The impact test of a material determines the shock resistance.(a) True(b) FalseThis question was addressed to me in a national level competition.Origin of the question is Impact Test in section Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Correct option is (B) False |
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| 15. |
The loading used for a homogenous specimen in the bucket’s hardness test is _______(a) 30kg(b) 500kg(c) 5kg(d) 13kgI have been asked this question during an online interview.This interesting question is from Aircraft Materials in portion Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Right answer is (a) 30kg |
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| 16. |
In the Charpy test, the notch faces _________ from the pendulum.(a) towards(b) 20m(c) away(d) aroundI have been asked this question in exam.This key question is from Aircraft Materials in section Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» RIGHT option is (c) away Easy explanation: In the Charpy test, the notch faces away from the pendulum. This differs from the other IMPACT test, the Izod impact test. This is one of the several DIFFERENCES between the TWO impact test methods. |
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| 17. |
Which of the following is a fatigue-testing apparatus?(a) Rotating-beam tests(b) Load test(c) Fixed load test(d) Rotating wing testThis question was posed to me during an interview.My enquiry is from Aircraft Materials topic in chapter Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Right option is (a) Rotating-beam TESTS |
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| 18. |
X-rays are typically powerful compared to gamma-rays which are weaker than X-rays.(a) True(b) FalseThis question was addressed to me in a national level competition.This question is from Testing Aircraft Materials in portion Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The correct option is (b) False |
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| 19. |
It is possible to determine the proof stress in a way in which ___________ is determined.(a) elastic limit(b) yield point(c) stress(d) strainThis question was posed to me in an international level competition.I'm obligated to ask this question of Aircraft Materials topic in division Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The correct answer is (a) ELASTIC limit |
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| 20. |
To find a true hardness reading for hard steel, the minimum thickness required for material is ____(a) 0.0027mm(b) 6.858mm(c) 0.27mm(d) 234mmThis question was posed to me by my school principal while I was bunking the class.My enquiry is from Aircraft Materials topic in chapter Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» RIGHT option is (B) 6.858mm To explain: To obtain the Rockwell hardness value, the loads used or penetrators DEPENDS on the weather the MATERIAL is soft or hard. The minimum thickness required for hard steel is 6.858mm. This will give an accurate hardness value. |
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| 21. |
A materials proof stress is the highest stress possible for it to tolerate without causing a permanent set of more than ___________ inch per inch the length of gage, after the total release of stress.(a) 5.1(b) 0.002(c) 0.0001(d) 0.1I got this question during an online interview.Query is from Aircraft Materials topic in division Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The CORRECT choice is (c) 0.0001 |
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| 22. |
To obtain consistent results in finding properties of materials, the specimen must be/have __________(a) no scratches(b) straightened(c) washed with methyl(d) bentI got this question by my school principal while I was bunking the class.My question is based upon Aircraft Materials in division Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» CORRECT CHOICE is (a) no SCRATCHES Best explanation: For the EXPERIMENT to work with the production of accurate results, the material must not contain scratches. It should not be STRAIGHTENED or bent as it will negatively affect the values of the experiment. |
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| 23. |
Flattening test is applied to __________(a) twisting(b) round steel wire(c) tubing(d) breakingI got this question in an interview for internship.This interesting question is from Aircraft Materials in portion Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Correct choice is (C) tubing |
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| 24. |
The specimen of fatigue testing must not have ___________(a) Uniform cross-section(b) Metal(c) Certain colours(d) Notches and holesI got this question in an international level competition.My question is from Aircraft Materials topic in chapter Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Correct CHOICE is (d) Notches and HOLES |
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| 25. |
The radius to which the jaws of the vice rounded to for wires of diameter less than 3/16 inches is _________(a) 2/15(b) 12/7(c) 3(d) 3/16I had been asked this question in homework.My question is from Aircraft Materials in portion Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Correct CHOICE is (d) 3/16 |
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| 26. |
The yield point can be determined in _____________(a) wood(b) carbon(c) pure molybdenum(d) mild carbon steelI got this question during an interview for a job.The above asked question is from Aircraft Materials topic in portion Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The CORRECT answer is (d) mild carbon steel |
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| 27. |
The yield point of a material does not exist for those materials that have a _____________ region in that space of the stress-strain curve.(a) smooth(b) shift(c) turbulent(d) highThis question was posed to me in homework.My question comes from Aircraft Materials topic in chapter Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The correct answer is (a) smooth |
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| 28. |
The shore scleroscope hardness test is carried out by ________ a tiny diamond-pointed hammer from a particular altitude and comparing the altitude of rebound to a standard test material.(a) inserting(b) cutting(c) smoothly pressing(d) droppingI have been asked this question during an interview.This key question is from Aircraft Materials topic in chapter Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The correct OPTION is (d) DROPPING |
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| 29. |
To perform Brinell test on a soft material like bronze _____________ kg of load is applied on the specimen.(a) 3000(b) 500(c) 6600(d) 1200The question was asked in an online quiz.This question is from Aircraft Materials topic in chapter Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Right option is (B) 500 |
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| 30. |
What is the rate of bending carried out for heavy wires?(a) 65 bending’s(b) 7 bending’s(c) 80 bending’s(d) 50 bending’sI had been asked this question in my homework.This interesting question is from Aircraft Materials in section Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The correct OPTION is (b) 7 BENDING’s |
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| 31. |
Fatigue stresses will most likely destroy the material if the bending test is performed on them.(a) True(b) FalseI had been asked this question by my school principal while I was bunking the class.I would like to ask this question from Aircraft Materials in chapter Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Right option is (b) False |
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| 32. |
In the flattening test, the length of the tubing is taken _________ times of the diameter.(a) 1(b) 2(c) 0.5(d) 4I have been asked this question in an interview for internship.My enquiry is from Aircraft Materials in portion Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The correct answer is (B) 2 |
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| 33. |
What is the principal use of the impact tests?(a) To determine ductility(b) To determine if the material has been subjected to heat treatment(c) To prevent material from corroding(d) To obtain absolute valuesI had been asked this question in class test.The origin of the question is Impact Test topic in division Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The correct choice is (b) To DETERMINE if the material has been subjected to heat treatment |
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| 34. |
If the bend of a bend test has to be gauged to its complete extent _________ of bend must be computed.(a) inner circumference(b) the inner minus outer circumference(c) outer circumference(d) inner radiusThe question was posed to me by my college director while I was bunking the class.I would like to ask this question from Aircraft Materials in portion Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Correct option is (c) outer circumference |
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| 35. |
If in an old test, energy absorbed (obtained on the scale) is 34 J and cross-section area of the notch is 10×8 mm square. What is the impact strength of the material?(a) 34 J per mm square(b) 4.25 J per mm square(c) 0.425 J per mm square(d) 80 J per mm squareI have been asked this question during an online exam.This intriguing question originated from Impact Test topic in portion Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Correct ANSWER is (c) 0.425 J per mm square |
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| 36. |
Which of the following can the inspection process ‘magnaflu’ not detect?(a) Laps(b) Cracks(c) Seams(d) ColorI got this question during an interview.My question is taken from Testing Aircraft Materials in division Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Right choice is (d) Color |
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| 37. |
What is the maximum speed up to which the clamp can be rotated in a torsion test?(a) 120rpm(b) 2rpm(c) -26rpm(d) 60rpmI got this question in an online interview.Asked question is from Aircraft Materials in chapter Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Right answer is (d) 60rpm |
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| 38. |
What is the continuous method of magnaflux inspection method?(a) The continuous specimen is used(b) Partial current mixing(c) Current is put on throughout the process(d) Non-existentThe question was posed to me by my college director while I was bunking the class.Asked question is from Testing Aircraft Materials in section Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The correct choice is (c) CURRENT is put on throughout the process |
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| 39. |
Fluoroscopy requires a higher voltage compared to radiography.(a) True(b) FalseThe question was posed to me by my college director while I was bunking the class.The above asked question is from Testing Aircraft Materials topic in section Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The CORRECT option is (a) True |
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| 40. |
Which of the following can be obtained through a tension test?(a) Colour(b) Heat treatment(c) Ultimate tensile strength(d) ConductivityThis question was addressed to me in an interview for job.My question is based upon Aircraft Materials topic in portion Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» CORRECT option is (c) Ultimate tensile strength Easy explanation: Tension TESTING can provide a lot of basic information about the property of the material being TESTED. Ultimate tensile strength is obtained through tension testing. It is the WITHSTANDING ability of a material to load. Tensile refers to bring pulled away. |
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| 41. |
What is the yield point of a material?(a) Change in the strain of a material(b) The ratio of proof stress to the area(c) The elasticity of a material(d) Point where there is a substantial increase in elongation without a rise in loadI got this question during an online exam.Asked question is from Aircraft Materials topic in section Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Correct answer is (d) POINT where there is a substantial increase in elongation WITHOUT a rise in load |
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| 42. |
Tension testing must be accurate within a percentage of ___________(a) +2%(b) +1%(c) +3/2 %(d) 21%I got this question in homework.This key question is from Aircraft Materials in section Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Right OPTION is (c) +3/2 % |
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| 43. |
The penetrator in the Vickers hardness test is a pyramid that is squarely based and has an included angle of _______(a) 206°(b) 15°(c) 136°(d) 23°This question was addressed to me in examination.This key question is from Aircraft Materials in portion Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The CORRECT choice is (c) 136° |
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| 44. |
For ____________ materials, there is no correspondence between tensile strength and hardness.(a) soft(b) hard materials(c) steel(d) carbonThe question was posed to me in examination.This key question is from Aircraft Materials in division Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Correct answer is (a) soft |
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| 45. |
_________ usually undergoes a reverse bend test.(a) Round steel wire(b) Glue(c) Plated iron(d) WoodThis question was posed to me in final exam.This interesting question is from Aircraft Materials in chapter Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Correct answer is (a) Round steel wire |
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| 46. |
The impact test value of a material changes with material.(a) True(b) FalseI got this question during a job interview.My enquiry is from Impact Test topic in section Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The CORRECT option is (a) True |
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| 47. |
The specimen used in the typical bend test (sheet) must have a width of _______ inches.(a) 12(b) 4(c) 1(d) 0.56I got this question in an international level competition.Question is from Aircraft Materials topic in portion Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Right answer is (c) 1 |
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| 48. |
The impact tests can be used to _____________(a) find out the absolute value of a material(b) to determine the tensile strength of a material(c) compare two specimens of similar composition and tensile strength(d) to find the quantity of materialThe question was asked at a job interview.I'm obligated to ask this question of Impact Test topic in chapter Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The correct CHOICE is (c) COMPARE TWO specimens of similar composition and TENSILE strength |
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| 49. |
The edges of a specimen of forging stock are rounded to a ________ radius in a bending test.(a) 20^th(b) 16^th(c) 1(d) 1/16^thThe question was asked in an interview.The above asked question is from Aircraft Materials in section Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The correct ANSWER is (d) 1/16^th |
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| 50. |
In the Charpy test, the tensile specimen being tested is ___________ on both sides.(a) threaded(b) axed(c) flattened(d) heatedThis question was addressed to me in a national level competition.I want to ask this question from Aircraft Materials in division Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Right option is (a) THREADED |
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