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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

Answer»

Right choice is (a) True

Explanation: The above statement is true. The magnaflux method ALSO DETECTS the location of flaws. This is because the powder on the specimen is disturbed as magnetic LINES of force are also disturbed in the location of the flaws.

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

Answer»

The correct CHOICE is (b) RADIOGRAPHY

Easiest explanation: Non-destructive testing way of materials refers to a process of inspection where the material is not DESTROYED or HARMED in any way. Radiography is a non-destructive way of inspecting materials.

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

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.
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

Answer»

The correct OPTION is (b) False

The best I can explain: Extensometer is an instrument used to measure the change in the length of a material. It should not be PLACED ANYWHERE to the SPECIMEN. It should be FIXED at the gage marks of the specimen being tested in the testing machine.

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

Answer»

The CORRECT answer is (c) proportional limit

For explanation: Proof stress of a material can also be called a proportional limit. The PROCEDURE to FIND the ELASTIC limit and proof stress are similar, but the quantities are different. Yield limit can be found through tension testing, but it is not the same as proof stress.

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

Answer»

Correct choice is (d) 8 KG per SQUARE millimeter

To elaborate: Brinell hardness number = \(\frac{Load \,APPLIED}{AREA \,of \,impression \,(spherical)}\)

= \(\frac{2000}{250}\)

= 8 kg per square millimeter.

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

Answer»

The correct answer is (b) energy

To elaborate: The Charpy test, like an Izod test, gives the energy ABSORBED by the specimen/MATERIAL being tested. This is used to obtain the comparative PROPERTIES of the desired MATERIALS. It also TELLS if the material is extremely brittle.

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

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.

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

Answer»

Right choice is (a) steel, diamond

To explain: ROCKWELL hardness value is found by calculating the penetration of either a steel ball or diamond cone under a particular LOAD. The Rockwell hardness NUMBER appears on the dial of the machine.

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

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.
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

Answer»

Correct choice is (d) demagnetized

Explanation: Some Aircraft MATERIALS TYPICALLY undergo the magnaflux INSPECTION process. After the inspection process is done the PARTS have to be demagnetized before being used for manufacturing. This is because otherwise, they will interfere with the plane’s compass.

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

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.
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

Answer»

The correct choice is (b) False

To explain I would SAY: There is typically no such particular requirement that the specimen of the BENDING test must be taken only PARALLEL to the grain. It is often REQUIRED for the specimen to be taken in both parallel and across the grain.

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

Answer»

The CORRECT answer is (c) TWISTING

For explanation: Torsion is defined as the twisting of a specimen caused by a CERTAIN AMOUNT of torque. COMPRESSIVE forces are forces that are applied to an object that results in the specimen getting compacted.

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

Answer»

Right option is (c) 30

To elaborate: The length required for a specimen of DIAMETER less than 0.033 inches in the torsion test is 30 inches. The length required for the wire being used in this experiment DEPENDS on the diameter of the specimen.

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

Answer»

The correct choice is (c) 8

To explain I would say: Gammagraphs of steel PARTS or materials as THICK as eight inches can also be acquired. This is higher COMPARED to RADIOGRAPHS with X-rays that can be used for steel as thick as only three inches.

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

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.
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

Answer»

The correct option is (a) Fixing a specimen in the machine to be broken by WEIGHT or heavy pendulum

Best EXPLANATION: An impact test is a procedure that INVOLVES notching a specimen on one side and FASTENING it to a machine to be broken, either by a SWINGING pendulum that is heavy or by a falling weight on it.

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

Answer»

The correct option is (b) False

The best I can EXPLAIN: This statement is not true. In the torsion TEST, steps are taken to ensure that kinking does not occur. The specimen is SUBJECTED to the required amount of tension so that kinking does not occur to affect the experiment.

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

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.
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

Answer»

Correct CHOICE is (b) False

The explanation: The statement is incorrect. Hardness testing machines don not GIVE the exact same results. Even if they are similar in TYPE, obtaining exact same results EVERY time is not possible.

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

Answer»

Right option is (a) True

The EXPLANATION is: A LOT of basic PROPERTIES of a material can be obtained through TENSION testing. It is an important test. ONE such property is the elongation of a material. It refers to the amount of increase in the length of a material.

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

Answer»

The correct CHOICE is (b) Black IRON OXIDE

To ELABORATE: It is necessary to put a substance on the specimen that can indicate the PRESENCE of flaws on it. Black iron oxide or ferroso ferric oxide is generally used as magnetic powder. They can be applied either wet or dry.

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

Answer»

The correct choice is (c) All directions

To explain I would say: It is important in the MAGNAFLUX INSPECTION method that the LINES of force (magnetic) GO through the defect perpendicularly. For this reason, since the location of defects is not know, it should be induced in all directions.

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

Answer»

Correct option is (b) Magnaflux

The BEST I can explain: The inspection METHOD is performed on MAGNETIC objects and used to determine cracks, LAPS, etc. On the material or part being inspected is called as magnaflux. Bending and fatigue are not inspection METHODS.

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

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.
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

Answer»

The correct answer is (C) Radiography and magnaflux INSPECTION

Explanation: It is materials being used in aircraft construction that should not experience failure while usage. HENCE, it is crucial for the materials to UNDERGO inspection to detect any cracks or defects. There are TWO standard inspection methods, they are radiography and magnaflux inspection.

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

Answer»

Right answer is (b) False

To explain I would SAY: The statement is not true. It is not at all easy to determine the fatigue stress of a MATERIAL. In fact, it is so difficult and consuming that there are lots of materials whose fatigue strength has not been FOUND.

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

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.
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

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.
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

Answer»

The correct option is (a) across

To EXPLAIN I would SAY: In the case of shop bending, it is usually preferred that all the bends be made across the grain. Once the test SPECIMEN passes the bending test, it is assured that the material is of good quality and there is a DIMINISHED possibility of CRACKING.

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

Answer»

The correct choice is (b) To OBTAIN accuracy

To explain: An EXTENSOMETER must be used in reading the permanent set. An accurate extensometer is REQUIRED to obtain the change in the property after the experiment is DONE, without any mistakes or problems with accuracy.

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

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.
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

Answer»

The correct option is (a) True

Explanation: There is a necessity to find the hardness of a MATERIAL as it can GIVE an indication of the strength and several other properties of a material. At the same time, it is important to AVOID damaging the material as that WOULD be a loss. Especially for a MANUFACTURED material.

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

Answer»

The correct answer is (c) SET method hardness

For explanation I WOULD say: Hardness testing methods are processes to check the strength of the material. Rockwell hardness, Brinell hardness, Shore scleroscope hardness and Diamond pyramid hardness are typically used hardness TESTS. The set method is one of the methods used to DETERMINE the yield strength of a material.

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

Answer»

Correct ANSWER is (c) Set

Easy EXPLANATION: The length AC is called the ‘set’ or GAGE length percentage. The graph REPRESENTS YIELD strength determination through the set method. The yield strength is represented at the point ‘B’ in the graph.

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

Answer»

Right answer is (b) False

Explanation: USUALLY, the PREFERRED method of determining yield strength can be used. It is not fixed. The two METHODS typically used to find the yield strength are set method and EXTENSION under load method.

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

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.
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

Answer»

Correct choice is (d) 0.5

To elaborate: The fatigue limit is different for different MATERIALS. For the MATERIAL steel, the fatigue limit is around 0.5 of its ultimate TENSILE strength. For materials that are non-ferrous in NATURE, the fatigue limit can 0.3 or 0.4 of its ultimate tensile strength.

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

Answer»

The correct answer is (a) lowest

The EXPLANATION: In an IZOD test, the material is first notched. Then it is clamped in heavy jaws, where the NOTCH level is with the top and facing the pendulum. After the pendulum is released from a CERTAIN height, it hits the material at the lowest point of its path.

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

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.
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

Answer»

Right choice is (d) 0.002

The BEST EXPLANATION: The extensions under load METHOD consists of two sections. First is elongation depending on the modulus of elasticity of object and expected yield strength and the second involves ADDING an extra elongation of 0.002 inch PER inch gage length.

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

Answer»

Right option is (d) the particular stress where a MATERIAL shows specified elongation under a load

The BEST explanation: The yield strength of a material is the particular stress where a material shows specified elongation under a load. The elongation of a material is the CHANGE in LENGTH before being affected by stress to after.

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

Answer»

Right choice is (B) 10^-6 to 10^-9 cm

For EXPLANATION I would say: Different types of rays are classified based on their respective wavelengths. The wavelength BRACKET in which the rays are considered to FIT the category of X-rays is from 10^-6 to 10^-9 centimeters.

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

Answer»

Correct option is (a) reduction

To explain I would SAY: Corrosion of a material is not a DESIRABLE quality. This is because even a small amount of it can cause a reduction of fatigue LIMIT. Even flaws like lack of uniform cross-section in the specimen can have the same effect.

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

Answer»

Correct option is (c) The amount of stress, a material can TOLERATE REPEATEDLY without failure

Easy explanation: The fatigue stress of a material is the stress it can tolerate several TIMES, without resulting in any failure. Each material has that fatigue stress and if it is CROSSED it is unsafe to load the material FREQUENTLY.

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

Answer»

Right answer is (a) True

For explanation I would SAY: This STATEMENT is true. In fact, it is true for both the Izod impact test and CHARPY impact test. Once the pendulum hits a specimen, it’s SWING decreases significantly DUE to interruption in its path.

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

Answer»

Right option is (d) 8

To elaborate: In the EXPERIMENTAL setup of the torsion TEST, there are two clamps PRESENT. The two clamps SECURE the wire in between them. The distance between the two camps in the machine is EIGHT inches.

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

Answer»

Right option is (a) 180°

Easiest explanation: The usual ANGLE with which the TEST specimen should be BENT in the bending test is 180°. This is over a pin that has the same diameter as that of the test specimen being used in the experiment. CRACKING should be AVOIDED.

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

Answer»

The correct option is (d) Charpy TEST

Best EXPLANATION: The method commonly preferred these days is the Charpy IMPACT test. The Izod impact test has ALSO been extensively used in the past. It is rarely used for testing materials/specimen these days.