Consider a body is subjected to some force F which is acting on cross section area of 10m^2. If stress due to application of the force is 25Pa then, found the value of F.(a) 250N(b) 1500N(c) 0.89KN(d) 890NI had been asked this question in a national level competition.My question comes from Structures Fundamentals in portion Structures and Loads of Aircraft Design

Consider a body is subjected to some force F which is acting on cross

1.	Consider a body is subjected to some force F which is acting on cross section area of 10m^2. If stress due to application of the force is 25Pa then, found the value of F.(a) 250N(b) 1500N(c) 0.89KN(d) 890NI had been asked this question in a national level competition.My question comes from Structures Fundamentals in portion Structures and Loads of Aircraft Design
Answer» Correct answer is (a) 250N The BEST EXPLANATION: FORCE or load = stress produced* cross section area = 25*10 = 250N.

Discussion

No Comment Found

Related InterviewSolutions

Following diagram represents _________(a) whisker reinforced composite(b) matrix only(c) fiber only(d) aluminum alloyI have been asked this question in final exam.I want to ask this question from Structures in chapter Structures and Loads of Aircraft Design
A column has effective length as 20unit. Determine Euler load of EI = 1000 unit.(a) 24.67 unit(b) 10 unit(c) 40 unit(d) 50.99 unitThe question was posed to me in final exam.This interesting question is from Structural-Analysis Fundamentals in portion Structures and Loads of Aircraft Design
Which of the following is an example of air load?(a) Gust(b) Taxi(c) Wheel stress(d) LandingThis question was posed to me in quiz.Enquiry is from Loads Categories topic in section Structures and Loads of Aircraft Design
The largest load that is expected to be experienced by aircraft is called __________(a) limit load(b) normal stress(c) normal strain(d) shear stressI have been asked this question in quiz.I need to ask this question from Loads Categories topic in portion Structures and Loads of Aircraft Design
Column has length of 1.2 m and radius of gyration as 1.5m. Determine slenderness ratio. Consider column is fixed at one end free at other end.(a) 1.6(b) 7.8(c) 98(d) 12.45I had been asked this question by my school principal while I was bunking the class.My question is taken from Structural-Analysis Fundamentals in division Structures and Loads of Aircraft Design
Determine the actual length of the column which has slenderness ratio of 2.9 and radius of gyration as 1.6. Consider column is fixed at both ends.(a) 9.28(b) 0.0045(c) 2.3674(d) 4.862The question was posed to me during a job interview.My doubt is from Structural-Analysis Fundamentals topic in chapter Structures and Loads of Aircraft Design
Following diagram represents ___________(a) v-n diagram combined of gust and Maneuver(b) v-n diagram landing(c) takeoff speed(d) drag coefficient vs liftThe question was asked in an interview for internship.The doubt is from Air Loads in division Structures and Loads of Aircraft Design
Magnesium is used for ________(a) control hinges(b) highest strength application(c) lofting(d) draftingI had been asked this question in class test.This interesting question is from Structures topic in division Structures and Loads of Aircraft Design
Composite material has only one material.(a) True(b) FalseI had been asked this question in quiz.The doubt is from Structures in division Structures and Loads of Aircraft Design
An object is subjected to some force. As a result of the force object undergoes in the deformation. If deformation of length is 0.28mm and Actual length is 20 mm then, find simple strain.(a) 0.014(b) 10.0014(c) 23.002(d) 0.00215The question was asked in my homework.The question is from Structures Fundamentals topic in chapter Structures and Loads of Aircraft Design

Discussion

No Comment Found

Related InterviewSolutions

Reply to Comment