My Report

Aircraft Design Mock Test 3


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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 10%

Question 1 of 10

1. Rolling tails can be used by high speed A/C.

Question 1 of 10

Question 2 of 10

2. As a designer, our job is to design a wing which has root chord Cr as 1m. What should be the approximate radius of fillet?

Question 2 of 10

Question 3 of 10

3. Following diagram represents ____
aircraft-design-questions-answers-conic-lofting-q6

Question 3 of 10

Question 4 of 10

4. Following diagram will generate _____________
aircraft-design-questions-answers-conic-fuselage-development-q8

Question 4 of 10

Question 5 of 10

5. If a wing has span of 12m. Find the approximated length of the aileron of starboard wing.

Question 5 of 10

Question 6 of 10

6. A wing is to be loft with span as 2m and reference area of wing is 4m2. If we want to design the wing with taper ratio of 0.6 then what will be the value of root chord?

Question 6 of 10

Question 7 of 10

7. Process of determining the take-off gross weight and required fuel weight is called as ________

Question 7 of 10

Question 8 of 10

8. Let’s consider we want to loft fuselage by using flat wrap method then, __________

Question 8 of 10

Question 9 of 10

9. What should be the load factor if, lift coefficient is designed as 2.1 and aircraft is operating at dynamic pressure q as 20 Pa. Given W/s =12.

Question 9 of 10

Question 10 of 10

10. If distance between shoulder point and tangent point is much higher then, it will produce ____________

Question 10 of 10


 

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.

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