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Aircraft Design Online Test


Correct Answer: 2 points | Wrong: -1 point
Grades: A* (100% score) | A (80%-99%) | B (60%-80%) | C (40%-60%) | D (0%-40%)
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Here is the complete list of test quizzes on Aircraft Design.

1. Following diagram represents _________
Graph representating estimation of the kinetic energy absorption at the time of braking

Question 1 of 50

2. For higher landing speed, deadrise angle should be __________

Question 2 of 50

3. If bypass ratio of subsonic non afterburning engine is found to be 2.1 then, what will be the specific fuel consumption of the same engine at cruise?

Question 3 of 50

4. As weight varies, rubber engine _______

Question 4 of 50

5. Short and fat fuselage will have ___________

Question 5 of 50

6. An aircraft has Crew and payload of 180kg. It has empty weight fraction of 0.48 and fuel weight is 0.7 times empty weight. What will be the gross weight of aircraft?

Question 6 of 50

7. Load factor is defined as _______________

Question 7 of 50

8. If aspect ratio of wing is 8 and S=0.1m2 then, what will be the span of wing?

Question 8 of 50

9. Which of the following is correct to trim an aircraft at positive AOA?

Question 9 of 50

10. Determine wing loading for civil aircraft if lift-off speed is 80m/s and maximum lift coefficient is 2.8.

Question 10 of 50

11. Which of the following is correct?

Question 11 of 50

12. Which of the following pair is correct based on the empty weight fraction?

Question 12 of 50

13. Consider turning gliding flight. Turn rate is given as 0.2 unit and velocity of flight is 10 unit. Find the value of turn radius.

Question 13 of 50

14. Following diagram represents ________
A power required graph representing altitude effects on the power

Question 14 of 50

15. Find the average velocity at transition if, stall speed is 15 unit.

Question 15 of 50

16. Which of the following is correct?

Question 16 of 50

17. The typical method for determining fuel weight used is called as _____

Question 17 of 50

18. Noise produced by an aircraft is called __________

Question 18 of 50

19. The inverted V-tail is used to ______

Question 19 of 50

20. Vulnerable area will be same for each and every aircraft.

Question 20 of 50

21. Buttock-planes are used to __________

Question 21 of 50

22. An aircraft with crew and payload of 180kg is flying. If fuel weight fraction is 0.353 and empty weight fraction 0.481 then, what will be the gross weight of aircraft?

Question 22 of 50

23. The purpose of the longitudinal control lines is __________

Question 23 of 50

24. If thickness ratio t/c is less or equal to the 0.05 then, the wetted area is ____

Question 24 of 50

25. We can provide sizing based on new design only.

Question 25 of 50

26. A seaplane has beam of 5 unit then, estimate the step size required for given seaplane.

Question 26 of 50

27. Following diagram represents _____
Figure representating intermediate step of conic lofting at ‘A’ and ‘B’ end points

Question 27 of 50

28. If sum of potential and kinetic energy of an aircraft is 5000 unit and aircraft weighs around 1200 unit then, determine specific total energy.

Question 28 of 50

29. We can minimize the weight of the structural member by _________

Question 29 of 50

30. Fuel tanks should not be located at wingtip.

Question 30 of 50

31. Seat reference point is the point where?

Question 31 of 50

32. Following diagram represents __________
Diagram representing high lift device(Flap) used to increase lift by wing during landing

Question 32 of 50

33. Stress and pressure are same.

Question 33 of 50

34. If area ratio is 1.110 then, at which mach number flow is flowing?

Question 34 of 50

35. If stall speed of the aircraft is 10m/s then, find the approximate value of takeoff speed.

Question 35 of 50

36. Supersonic wave drag can be reduced by using ____________

Question 36 of 50

37. Elevator control power is given by _____

Question 37 of 50

38. Which of the following is an advantage of internal weapon carriage?

Question 38 of 50

39. Which weapon carriage option gives more flexibility to carry different weapons?

Question 39 of 50

40. Following diagram represents _________
Whisker reinforced composite material

Question 40 of 50

41. If load factor of level turning flight is found to be 1.2 and flight speed is 120m/s then, determine turn rate.

Question 41 of 50

42. Which of the following is correct?

Question 42 of 50

43. We are using the airfoil in the aircraft as _____

Question 43 of 50

44. Stroke of a shock absorber is defined as _________

Question 44 of 50

45. An aircraft is designed to be in steady level flight with weight of 1500N and CL of 1.0. Determine at which speed we need to design this aircraft so that it can achieve this requirement. Consider density as 1.2 kg/m3 and reference area as 2m2.

Question 45 of 50

46. Following diagram represents ___________
A typical combined V-n diagram of gust and Maneuver

Question 46 of 50

47. A supersonic aircraft is designed to operate at 2.0M if thrust loss is required to be less than 2% then determine the reference value of inlet pressure recovery. Given ram recovery Correction factor C is 1.2.

Question 47 of 50

48. A twin turboprop engine is flying with 120m/s. Wing of the aircraft has span of 2m and lift co-efficient as 0.15 with aspect ratio as 9.2. Find the lift produced by the wing.

Question 48 of 50

49. Inflow ratio is defined as __________

Question 49 of 50

50. Following diagram represents ____
Diagram representating location of sub-assembly breaks causing problems during production

Question 50 of 50


 

Topic wise Test Quizzes on Aircraft Design

Aircraft Design tests, quizzes, and exams are great ways to learn and test your Aircraft Design skills. Whether you’re a beginner or experienced, challenge and boost your confidence with our engaging online quizzes on Aircraft Design Basics, Conceptual Sketch Sizing, Airfoil Selection, Wing Loading, Aircraft Design Initial Sizing, Aircraft Configuration Layout, Aircraft Propulsion, Jet Engine Performance, Aircraft Structure, Aircraft Stability, Flight Mechanics, and Aircraft Operation. Start the Aircraft Design online test now!

Aircraft Design Basic Quiz

Conceptual Sketch Sizing Quiz

Airfoil Selection Quiz

Geometry Selection Quiz

Wing Loading Quiz

Aircraft Design Initial Sizing Quiz

Aircraft Configuration Layout Quiz

Aircraft Propulsion Quiz

Aircraft Landing Gear Quiz

Jet Engine Performance Quiz

Aircraft Structure Quiz

Aircraft Stability Quiz

Flight Mechanics Quiz

Aircraft Operation Quiz


Aircraft Design Certification Test

Aircraft Design Certification Test is a free certification exam. However, you need to score an A grade in each of the "Certification Level Tests 1 to 10" to be eligible to take part in this certification test. So, take all the "10 Tests" starting from Certification Level 1 upto Level 10, before taking the final Certification test.

Level 1 Test Certification Test

Level 1 to 10 Tests:
Total Questions: 25, Total Time: 30 min, Correct Answer: 2 points, Wrong Answer: -1 point

Certification Test:
Total Questions: 50, Total Time: 1 hour, Correct Answer: 2 points, Wrong Answer: -1 point

Aircraft Design Internship Test

If you scored either Grade A* or Grade A in our Aircraft Design Internship Test, then you can apply for Internship at Sanfoundry in Aircraft Design.

Aircraft Design Internship Test

Total Questions: 50, Total Time: 1 hour, Correct Answer: 2 points, Wrong Answer: -1 point

Aircraft Design Job Test

It is designed to test and improve your skills for a successful career, as well as to apply for jobs.

Aircraft Design Job Test

Total Questions: 50, Total Time: 1 hour, Correct Answer: 2 points, Wrong Answer: -1 point

Note: Before you get started on these series of online tests, you should practice our collection of 1000 MCQs on Aircraft Design .

Sanfoundry Scoring & Grading System

Sanfoundry tests and quizzes are designed to provide a real-time online exam experience. Here is what you need to know about them.

  • Scoring System: You get 2 points for each correct answer but lose 1 point for every wrong answer.
  • Grading System: Your grade depends on your final score and can be one of the following:

    • Grade A* - Genius (100%)
    • Grade A - Excellent (80% to 99%)
    • Grade B - Good (60% to 80%)
    • Grade C - Average (40% to 60%)
    • Grade D - Poor (0% to 40%)
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Manish Bhojasia - Founder & CTO at Sanfoundry
Manish Bhojasia, a technology veteran with 20+ years @ Cisco & Wipro, is Founder and CTO at Sanfoundry. He lives in Bangalore, and focuses on development of Linux Kernel, SAN Technologies, Advanced C, Data Structures & Alogrithms. Stay connected with him at LinkedIn.

Subscribe to his free Masterclasses at Youtube & discussions at Telegram SanfoundryClasses.