Explore topic-wise InterviewSolutions in .

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

Answer»

Correct choice is (a) 5

The explanation: The shore scleroscope number is obtained by conducting the EXPERIMENT 5 times and taking an average of the obtained 5 values. The FINAL obtained average VALUE is considered shore scleroscope number.

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

Answer»

Right ANSWER is (b) 5 inch per inch gage length

To EXPLAIN: The FORMULA of normal ELONGATION is given by = \(\frac{Expected \, yield\, strength}{Modulus \,of\, ELASTICITY}\)

= \(\frac{50,000}{10,000}\)

= 5 inches per inch gage length.

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

Answer»

Right choice is (c) 1 INCH

For explanation I WOULD say: Specimen of fatigue TESTS are typically rolled or forged bar stock. The are ONE inch in diameter. They can vary depending on the REQUIREMENTS and the material being tested to determine fatigue strength.

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

Answer»

The CORRECT choice is (b) False

To explain: It is not very effortless or easy to OBTAIN the exact desired radius of bending in the bending test being performed. But this test can OFTEN be used in shops etc. to check the PROPERTIES of the material if there is a doubt about them.

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

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.
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

Answer»

The CORRECT option is (c) 18 inches

Easy EXPLANATION: There are TWO methods of demagnetization. One of the methods involves withdrawing the specimen to a distance of eighteen inches away from the coil. This is to avail the EFFECT of the weak current.

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

Answer»

Correct answer is (d) time-consuming

Explanation: There are a lot of ADVANTAGES and DISADVANTAGES of standard inspection METHODS. When it COMES to radiography, one of the disadvantages is that it can be time-consuming. It also needs PHOTOGRAPHY.

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

Answer»

Right ANSWER is (a) normal

Explanation: The material or the specimen should be positioned in true axial alignment. This is considered vital, ESPECIALLY since materials used in aircraft construction are thin. This will avoid DAMAGING them.

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

Answer»

Right choice is (c) 1/16

To elaborate: The crosshead of the tension TESTING MACHINE has a certain advisable LIMIT in speed it has to be operated up to. It is different until the yield point and after yield point TILL RUPTURE. Until yield point it is 1/16 inch, yield point to rupture it is 1/2 inch. (Inch per inch)

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

Answer»

The correct answer is (a) 0.0003

Best explanation: For a LENGTH of one inch, the PERMANENT SET of over 0.0001 inch withstanding is proof stress. For 3 INCHES length, it will be –

0.0001×3 = 0.0003 inches.

Hence, it is 0.0003 inches.

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

Answer»

The correct answer is (a) True

The best EXPLANATION: Tension TESTING can give us crucial information REGARDING the properties of a material. Apart from the ultimate tensile strength, the yield strength and reduction in AREA can be DETERMINED through tension testing.

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

Answer»

The CORRECT ANSWER is (a) no necessity to plot a curve

Explanation: The extension under load method is USED much more than the set method. This is due to the fact that the former method does not require the plotting of a curve to find the yield STRENGTH of a material.

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

Answer»

The CORRECT choice is (a) 3

The best EXPLANATION: In a flattening test, the maximum limit up to which the THICKNESS of the tube can be considered is THREE TIMES the thickness of the wall. This is in the case of bronze tubing in flattening test.

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

Answer»

Correct option is (B) False

The explanation is: The STATEMENT is not true as the IMPACT test does not determine the shock resistance of the particular material. The impact test can indicate if the material is extremely BRITTLE. It also tells US if a material has undergone the right heat treatment or not.

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

Answer»

Right answer is (a) 30kg

To EXPLAIN: In the Vickers/diamond hardness test, the AMOUNT of LOAD applied typically on homogenous material is 30kg. 5kg is the weight applied to materials that are soft or those that have a hard SURFACE.

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

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.
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

Answer»

Right option is (a) Rotating-beam TESTS

Easy explanation: There are several different types of fatigue testing apparatus AVAILABLE to test MATERIALS or specimen. But the most widely USED apparatus is rotating-beam tests also called as rotating-cantilever tests.

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

Answer»

The correct option is (b) False

Best explanation: This statement is INCORRECT. X-rays are not stronger COMPARED to gamma-rays. In fact, the CONTRARY is true. X-rays are weak compared to gamma-rays, due to which gamma-rays can be used to inspect materials of greater thickness.

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

Answer»

The correct answer is (a) ELASTIC limit

To ELABORATE: The proof stress of a MATERIAL can be found or determined the same way the elastic limit can be determined. But, there are other methods through which the elastic limit can be found as well.

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

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.
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

Answer»

The CORRECT choice is (c) 0.0001

For explanation: The highest possible stress a material can, WITHOUT causing a permanent SET of more than 0.00001 inch per inch of the gage length is called PROOF stress. This is after the total release of the stress.

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

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.
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

Answer»

Correct choice is (C) tubing

Easy explanation: Flattening test is typically APPLICABLE for tubing. ROUND steel wire generally undergoes reverse bend test. Both of these are methods used to find the nature of the material, more SPECIFICALLY the ductility.

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

Answer»

Correct CHOICE is (d) Notches and HOLES

The best I can explain: It is NECESSARY that the specimen being tested to determine fatigue strength not have notches and holes in it. The specimen is usually cylindrical rods that do not CONTAIN any of the above defects.

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

Answer»

Correct CHOICE is (d) 3/16

The best I can explain: If the diameter of the wire in which the test is being carried out is less than 3/16 inches of diameter, the JAWS of the VICE are rounded to 3/16 inches. For wires of GREATER weight, the vice is SET to 3 times the diameter of the wire.

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

Answer»

The CORRECT answer is (d) mild carbon steel

Easiest explanation: The YIELD point is not present in all available materials. It is present in certain materials like Mild carbon steel and wrought IRON. It does not EXIST in wood, pure carbon or pure molybdenum. There are two methods to determine the yield point of a material.

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

Answer»

The correct answer is (a) smooth

Easiest explanation: The materials that have a SHARP break in the yield point of the stress-strain curve tend to have a yield point. These are materials LIKE WROUGHT IRON. Other materials have a smooth REGION in the place of the sharp break of yield point, hence do not have this property.

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

Answer»

The correct OPTION is (d) DROPPING

The BEST I can explain: This hardness test is carried out by comparing the rebound ALTITUDE of the test material after dropping a TINY diamond pointed hammer on the test specimen, to that of a standard test material.

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

Answer»

Right option is (B) 500

Easy explanation: Different amount of load are applied on test specimen depending UPON the TYPE of MATERIAL being tested. For steel testing, the pressure applied is 3000kg. For comparatively softer MATERIALS like aluminium alloys, the pressure applied is 500kg.

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

Answer»

The correct OPTION is (b) 7 BENDING’s

Easiest explanation: For heavy wire, the RATE of bending in the reverse bend test is 7 bends per MINUTE. For SMALL wire, the rate of bending in the experiment is fifty bends per minute. This is the specification given.

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

Answer»

Right option is (b) False

To elaborate: The bending TEST being performed on the test specimen is to GAUGE the ductility of the material. Once the test is performed, if the specimen has passed the test, it means that the material is most LIKELY not going to be destroyed due to fatigue STRESSES.

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

Answer»

The correct answer is (B) 2

The explanation: The FLATTENING test is generally APPLIED for tubing. It gives an idea about the ductility of the material. In this test, the LENGTH of the TUBE is taken as two times the diameter. It is flattened in a sideways direction and scrutinized to detect any defects.

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

Answer»

The correct choice is (b) To DETERMINE if the material has been subjected to heat treatment

Explanation: The PRINCIPAL or main reason that the impact TEST is conducted upon a material is to ASCERTAIN if the material has undergone the required accurate heat treatment. The experiment gives no absolute value.

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

Answer»

Correct option is (c) outer circumference

The best I can explain: If we desire to OBTAIN the complete EXTENT of the bending TEST being performed, it is necessary to compute the BEND of the outer circumference of the test SPECIMEN in the experiment.

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

Answer»

Correct ANSWER is (c) 0.425 J per mm square

For explanation I would say: Formula for impact strength = \(\frac{Energy \,absorbed}{Cross-section \,AREA \,of \,NOTCH}\)

= \(\frac{34}{10×8}\)

= 0.425 J per mm square.

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

Answer»

Right choice is (d) Color

To explain: MAGNAFLUX is a magnetic inspection METHOD USED to detect defects and non-metallic quantities in a magnetic material. It can detect CRACKS, seams etc. but cannot detect COLOUR of the specimen.

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

Answer»

Right answer is (d) 60rpm

To explain I WOULD say: The torsion TEST experimental set up contains TWO clamps. One is rotatable and the other FIXED. The rotatable clamp is moved at a rate of 60rpm (rotations per minute) at maximum. This is because exceeding that speed MIGHT cause heating.

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

Answer»

The correct choice is (c) CURRENT is put on throughout the process

To explain: The continuous METHOD of magnaflux involves inducing both CIRCULAR and longitudinal current at the same time and RUNNING it throughout the entire process. This is known to give good RESULTS.

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

Answer»

The CORRECT option is (a) True

For explanation: The above STATEMENT is true. Fluoroscopy is a method of non-destructive INSPECTION that has been DEVELOPED after radiography. It REQUIRES a higher voltage compared to radiography to perform.

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

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.
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

Answer»

Correct answer is (d) POINT where there is a substantial increase in elongation WITHOUT a rise in load

The best I can explain: A materials yield point is the point where there is a significant increase in the elongation without an increment in the load. The yield point of a material can be DETERMINED in two WAYS – the divider method, and DROP of beam method.

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

Answer»

Right OPTION is (c) +3/2 %

To elaborate: The process of tension testing MUST adhere to certain conditions to ASSURE its validity. ONE of the conditions is the RANGE of accuracy of the testing machine. The percentage within which the accuracy should be present is 3/2%.

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

Answer»

The CORRECT choice is (c) 136°

To elaborate: The INCLUDED angle of the square based, pyramid diamond PENETRATOR in the Vickers/diamond HARDNESS TEST is 136°. 15° and 23° would be too low of an angle to be considered.

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

Answer»

Correct answer is (a) soft

To explain: There is a relation between hardness and tensile strength for MATERIALS like CARBON and low alloy steels. The tensile strength can be PREDICTED USING hardness values. But for comparatively soft materials like ALUMINIUM alloys, this is not applicable.

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

Answer»

Correct answer is (a) Round steel wire

Best EXPLANATION: Round steel wire is USUALLY the most widely used specimen while performing the REVERSE BEND TEST in laboratories. Wood and glue cannot be used or have the bending test performed on them.

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

Answer»

The CORRECT option is (a) True

For explanation I would say: The IMPACT test value can change with change in temperature. For EXAMPLE, consider an impact test conducted at a low temperature. The impact test value DECREASES. Hence with a decrease in temperature, the impact energy is reduced.

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

Answer»

Right answer is (c) 1

Explanation: The specimen being used in the bending test, if it’s a sheet or strip STOCK TYPICALLY has a width of ONE inch. The general length of the specimen considered is six INCHES. The edges of the specimen should not contain ROUGH spots.

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

Answer»

The correct CHOICE is (c) COMPARE TWO specimens of similar composition and TENSILE strength

The EXPLANATION: The impact test can be used to compare two specimens that have a similar composition and tensile strength. It has no absolute value. The test used to determine the tensile strength of a material is the tension test.

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

Answer»

The correct ANSWER is (d) 1/16^th

The best EXPLANATION: The specimens of forging stock ALSO undergo the bending TEST. They are machined to a minimum of six inches in length. Their edges are rounded to a one by sixteenth radius. It differs for heavy material.

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

Answer»

Right option is (a) THREADED

Explanation: The tensile specimen in the CHARPY impact test is threaded on both SIDES. One of the ends is threaded to the pendulum that is swinging. It is not axed, heated or subjected to any such TREATMENT before being tested.