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.
| 51. |
Not only the presence of defects, but their location can also be known in the magnaflux inspection process.(a) True(b) FalseThis question was posed to me in an interview.This is a very interesting question from Testing Aircraft Materials in division Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Right choice is (a) True |
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| 52. |
Which of the following is a non-destructive way of inspecting materials?(a) Fatigue(b) Radiography(c) Welding(d) BendingThis question was posed to me at a job interview.This intriguing question comes from Testing Aircraft Materials in division Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The correct CHOICE is (b) RADIOGRAPHY |
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| 53. |
It is vital that surfaces that have to be tested to determine the hardness of the material must be free of _____(a) ridges(b) evenness(c) smoothness(d) thicknessThis question was posed to me in class test.My question is based upon Aircraft Materials in chapter Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» CORRECT option is (a) RIDGES For explanation I would say: In order to perform tests on the material, it must meet CERTAIN standards. It should have the required thickness to AVOID bulging and must be free of ridges and SCRATCHES. It should be even and smooth. |
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| 54. |
The extensometer can be attached anywhere to the specimen.(a) True(b) FalseThis question was posed to me by my college director while I was bunking the class.This intriguing question comes from Aircraft Materials topic in division Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The correct OPTION is (b) False |
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| 55. |
A materials proof stress is also referred to as ___________(a) elastic limit(b) yield limit(c) proportional limit(d) set methodThe question was asked in examination.Origin of the question is Aircraft Materials in chapter Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The CORRECT answer is (c) proportional limit |
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| 56. |
If the load being applied is 2000kg, and the area of impression is 250 Square millimetres, what is the Brinell number of the test material?(a) 80 kg per square millimeter(b) 25 kg per square millimeter(c) 20 kg per square millimeter(d) 8 kg per square millimeterI have been asked this question by my college professor while I was bunking the class.My doubt is from Aircraft Materials in chapter Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Correct choice is (d) 8 KG per SQUARE millimeter |
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| 57. |
The Charpy test, which is a type of impact test measures the __________ absorbed by a specimen.(a) heat(b) energy(c) length(d) breadthThis question was posed to me in an internship interview.Query is from Aircraft Materials topic in section Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The correct answer is (b) energy |
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| 58. |
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 |
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Answer» Correct OPTION is (b) 500,000,000 |
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| 59. |
Rockwell hardness test uses either a ____________ ball or ___________ cone for measuring hardness.(a) steel, diamond(b) diamond, steel(c) carbon, iron(d) iron, carbonThe question was posed to me in my homework.Origin of the question is Aircraft Materials in section Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Right choice is (a) steel, diamond |
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| 60. |
The elastic limit of a material is _____________(a) the least amount of stress that can be held without permanent deformation(b) highest stress a material can experience without permanent deformation(c) average stress experienced by material in its lifeline.(d) strain on materialThe question was asked in homework.I want to ask this question from Aircraft Materials topic in section Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» CORRECT option is (B) highest stress a material can experience without permanent deformation To explain: The ELASTIC LIMIT is the highest stress that a material can withstand, without permanent deformation present when the stress is RELEASED completely. It is not the lowest amount of stress present. |
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| 61. |
Before sending the material that is being inspected to construct an aircraft, it has to be ___________(a) washed(b) compressed(c) liquefied(d) demagnetizedThis question was posed to me during an internship interview.Question is taken from Testing Aircraft Materials topic in chapter Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Correct choice is (d) demagnetized |
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| 62. |
In the tension testing experiment, while determining elastic limit, the increment, while the load is being increased, should not exceed ___________ % of the elastic limit in the ending.(a) 50(b) 7(c) 2(d) 3The question was posed to me in final exam.My question is based upon Aircraft Materials in portion Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» RIGHT option is (d) 3 For explanation: In the tension TESTING experiment, we can determine the elastic limit. Here the load is applied gradually in different points to determine the elastic limit. In the final part of the experiment, the load being INCREASED should not exceed 3% of the elastic limit. |
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| 63. |
The specimen of the bending test must be taken only parallel to the grain.(a) True(b) FalseI had been asked this question in class test.This is a very interesting question 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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| 64. |
“Torsion” is defined as _________(a) compressive force(b) type of friction(c) twisting(d) object at restI got this question in an interview for internship.I would like to ask this question from Aircraft Materials topic in portion Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The CORRECT answer is (c) TWISTING |
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| 65. |
If a wire that has a diameter of less than 0.033 inches has to undergo a torsion test, the length of the specimen being used must be _________ inches.(a) 10(b) 100(c) 30(d) 8I got this question during an interview.My query is from Aircraft Materials in portion Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Right option is (c) 30 |
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| 66. |
Gammagraphs of steel that is as thick as ___________ inches can be acquired.(a) 4(b) 31(c) 8(d) 15The question was asked in exam.The origin of the question is Testing Aircraft Materials topic in section Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The correct choice is (c) 8 |
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| 67. |
The fatigue limit of a specimen is ___________ of its fatigue range.(a) triple(b) double(c) half(d) exactly the sameI had been asked this question in unit test.My question is based upon Aircraft Materials in division Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» RIGHT answer is (c) half The EXPLANATION: The FATIGUE LIMIT of a specimen or material is half of its fatigue RANGE. The fatigue value of a material also depends on load, but it will typically be in the fatigue range for materials or specimen. |
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| 68. |
What is an impact test?(a) Fixing a specimen in the machine to be broken by weight or heavy pendulum(b) Indenting with the help of a diamond hammer(c) Rolling with steel(d) Dipping in a mixture of ethanol and carbon and checking indentation of a materialThis question was addressed to me at a job interview.I'd like to ask this question from Impact Test topic in portion Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The correct option is (a) Fixing a specimen in the machine to be broken by WEIGHT or heavy pendulum |
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| 69. |
The wire constantly experiences kinking when it is subjected to the torsion test.(a) True(b) FalseThe question was posed to me during an internship interview.This question is from Aircraft Materials topic in division Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The correct option is (b) False |
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| 70. |
The maximum rate up to which bending is done per minute is ________ in reverse bend test.(a) 35(b) 5(c) 50(d) 26I got this question in an online quiz.My question is taken from Aircraft Materials in division Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» RIGHT option is (c) 50 To explain I would say: The maximum speed up to which the bending EXPERIMENT can be CONDUCTED in the reverse band test is 50 bends per minute. This should be DONE while considering how it could be PRONE to heating. |
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| 71. |
Similar hardness testing machines give the exact same results.(a) True(b) FalseThis question was addressed to me in my homework.The doubt is from Aircraft Materials topic in portion Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Correct CHOICE is (b) False |
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| 72. |
The elongation of a material can be obtained through tension testing.(a) True(b) FalseThis question was addressed to me during an online exam.My question is taken from Aircraft Materials topic in chapter Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Right option is (a) True |
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| 73. |
_____________ can be put on the specimen in the form of magnetic powder.(a) Uranium(b) Black iron oxide(c) Charred wood(d) ChromiumI have been asked this question by my school principal while I was bunking the class.The question is from Testing Aircraft Materials topic in division Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The correct CHOICE is (b) Black IRON OXIDE |
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| 74. |
In which direction should the magnetic flux be induced on the specimen?(a) Upper(b) Lower(c) All directions(d) NorthThe question was asked in an online quiz.Question is from Testing Aircraft Materials in division Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The correct choice is (c) All directions |
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| 75. |
___________ is an inspection method for magnetic objects(a) Fatigue(b) Magnaflux(c) Gammagraphs(d) BendingI had been asked this question in a national level competition.The above asked question is from Testing Aircraft Materials in section Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Correct option is (b) Magnaflux |
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| 76. |
Gamma-rays are acquired from ___________(a) Radiograph(b) X-ray(c) U.V(d) RadiumI have been asked this question by my school principal while I was bunking the class.I would like to ask this question from Testing Aircraft Materials in chapter Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» RIGHT choice is (d) Radium For EXPLANATION: Gamma-RAYS are acquired from radium. It is typically in radium sulphate FORM. Gamma-rays are rays having a wavelength of around 10^-11centimeters. It TAKES radium 1580 years to decay to one-half it’s original strength. |
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| 77. |
Which of the following are standard inspection methods of aircraft materials?(a) Radiography and fatigue test(b) Magnaflux and bending inspection(c) Radiography and magnaflux inspection(d) Fatigue and bending inspectionI have been asked this question in unit test.This interesting question is from Testing Aircraft Materials topic in section Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The correct answer is (C) Radiography and magnaflux INSPECTION |
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| 78. |
Testing a material to know it’s fatigue strength is very easy.(a) True(b) FalseThe question was asked in an online interview.Enquiry is from Aircraft Materials topic in chapter Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Right answer is (b) False |
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| 79. |
In the torsion test, there are two clamps. The clamps are _________(a) both fixed(b) one fixed one rotating(c) both rotating(d) both joined permanentlyThe question was asked in an interview.Origin of the question is Aircraft Materials in division Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» RIGHT answer is (b) ONE fixed one rotating To ELABORATE: There are two clamps present in the experimental SET up of the torsion test. One of the clamps is fixed while the other one is ROTATABLE. In the experiment, the rotatable clamp is moved at a certain speed. |
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| 80. |
Which of the following affects a Charpy test?(a) Specimen gauges factor(b) Test machine frequency(c) Colour(d) Yield strengthI got this question in an interview for job.I'd like to ask this question from Aircraft Materials topic in portion Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» RIGHT choice is (d) Yield strength The explanation: Several factors affect a CHARPY impact TEST. Some of them INCLUDE TEMPERATURE, yield strength and fracture mechanisms. But the factors like colour and other irrelevant quantities are not important. |
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| 81. |
It is usually preferred for shop bending to take all the present bends ________ grain.(a) across(b) above(c) below(d) parallelThe question was posed to me at a job interview.Asked question is from Aircraft Materials topic in division Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The correct option is (a) across |
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| 82. |
Why must an accurate extensometer be used in reading a permanent set?(a) It is cheap(b) To obtain accuracy(c) It is radioactive(d) It is unnecessaryThis question was addressed to me by my school teacher while I was bunking the class.I'd like to ask this question from Aircraft Materials topic in division Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The correct choice is (b) To OBTAIN accuracy |
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| 83. |
In the Brinell testing method, the load should be pressed for a minimum of ____________(a) 1000 seconds(b) 60 seconds(c) 10 seconds(d) 3 secondsThis question was posed to me during an interview.Enquiry is from Aircraft Materials in portion Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» CORRECT OPTION is (c) 10 seconds Best explanation: In the Brinell testing method, the TEST specimen is indented with a ball MADE of steel, with a diameter or 10 mm for a certain amount of time. The minimum time period is 10 seconds before the LOAD is released. |
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| 84. |
There is a necessity to find the hardness of a material without causing deformation in them.(a) True(b) FalseI got this question in an interview for job.My question comes from Aircraft Materials topic in chapter Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The correct option is (a) True |
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| 85. |
Which of the following is not a hardness testing method?(a) Rockwell hardness(b) Brinell hardness(c) Set method hardness(d) Shore scleroscope hardnessThe question was posed to me during an interview for a job.My question is from Aircraft Materials in division Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The correct answer is (c) SET method hardness |
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| 86. |
What does length ‘AC’ in the diagram represent?(a) Yield gage(b) Yield strength(c) Set(d) Yield pointThis question was posed to me in a national level competition.The above asked question is from Aircraft Materials topic in portion Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Correct ANSWER is (c) Set |
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| 87. |
There is often no choice between the two methods of determination of yield strength available, as it is predetermined.(a) True(b) FalseThe question was posed to me in class test.I'd like to ask this question from Aircraft Materials in division Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Right answer is (b) False |
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| 88. |
When radiographs are produced to detect defects, they show up as ___________(a) tubes(b) dark spots(c) invisible spots(d) light spotsThe question was posed to me by my college professor while I was bunking the class.My doubt is from Testing Aircraft Materials in portion Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» CORRECT choice is (d) light SPOTS To explain I would say: RADIOGRAPHY is a non-destructive METHOD of inspecting materials. It is performed by passing either X-rays or gamma-rays through the MATERIAL being tested. Defects or cracks are obtained in the picture in the form of light spots. |
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| 89. |
The fatigue limit of steel is around ____ times the ultimate tensile strength.(a) 0.3(b) 5(c) 3(d) 0.5This question was posed to me by my college director while I was bunking the class.This interesting question is from Aircraft Materials topic in division Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Correct choice is (d) 0.5 |
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| 90. |
In an Izod test after the pendulum is released from a certain height, it hits the material at the __________ point of it’s path.(a) lowest(b) opposite(c) highest(d) sidewaysI have been asked this question in an interview for job.This intriguing question comes from Impact Test topic in chapter Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The correct answer is (a) lowest |
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| 91. |
It is impossible to find a relation between hardness and tensile strength.(a) True(b) FalseI have been asked this question during an online exam.My question is based upon Aircraft Materials topic in section Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» RIGHT answer is (B) False Easiest EXPLANATION: There is a relation between the hardness and tensile strength. The APPROXIMATE value of the tensile strength of several materials can be FOUND when the hardness of those materials is known. |
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| 92. |
The second part of specified extensions in the extensions under load method typically involves adding an elongation of ____ inch per inch of gage length.(a) 0.2(b) 2.02(c) 0.02(d) 0.002This question was addressed to me during a job interview.The above asked question is from Aircraft Materials topic in portion Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Right choice is (d) 0.002 |
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| 93. |
The yield strength of a material is ___________(a) the proof stress of a material(b) the strain where the strength of material fails(c) the elongation(d) the particular stress where a material shows specified elongation under a loadI had been asked this question during a job interview.The origin of the question is Aircraft Materials topic in portion Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Right option is (d) the particular stress where a MATERIAL shows specified elongation under a load |
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| 94. |
What wavelengths are classified as X-rays?(a) 10^-6 to 10^-25 cm(b) 10^-6 to 10^-9 cm(c) 10^-2 to 10^-9 cm(d) 25 to 15cmI have been asked this question in my homework.This question is from Testing Aircraft Materials topic in section Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Right choice is (B) 10^-6 to 10^-9 cm |
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| 95. |
Corrosion of materials results in ___________ of fatigue limit.(a) reduction(b) increment(c) double(d) satisfactionI had been asked this question at a job interview.This interesting question is from Aircraft Materials in division Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Correct option is (a) reduction |
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| 96. |
What is fatigue stress?(a) The stress endured by an observer(b) Stress divided by strain and multiplied by conductivity(c) The amount of stress, a material can tolerate repeatedly without failure(d) The stress endured perpendicular to the observerThe question was asked during an online interview.This key question is from Aircraft Materials in section Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Correct option is (c) The amount of stress, a material can TOLERATE REPEATEDLY without failure |
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| 97. |
The swing of a pendulum/hammer decreases after it comes in contact with the specimen in a Charpy test.(a) True(b) FalseI got this question in semester exam.Question is from Aircraft Materials topic in section Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Right answer is (a) True |
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| 98. |
The setup of a torsion test involves two clamps having a distance of _________ inches between them.(a) 10(b) 18(c) 26(d) 8This question was posed to me in quiz.I'm obligated to ask this question of Aircraft Materials in division Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Right option is (d) 8 |
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| 99. |
The usual angle through which bending should be obtained in a bending test is ________(a) 180°(b) 120°(c) 75°(d) 90°This question was addressed to me during an internship interview.The doubt is from Aircraft Materials topic in section Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» Right option is (a) 180° |
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| 100. |
Which of the following impact test method is preferred these days?(a) Impact test(b) Reverse bend test(c) Flattening test(d) Charpy testI have been asked this question in final exam.Question is from Aircraft Materials in portion Testing Aircraft Materials of Aerospace Materials & Processes |
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Answer» The correct option is (d) Charpy TEST |
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