Aircraft Design - - Unit 8 - Week - 7
https://onlinecourses.nptel.ac.in/noc17_ae08/unit?unit=58&assessment=66 1/2
Courses » Aircraft Design
Unit 8 - Week - 7
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2 points 1)
2 points 2)
2 points 3)
Assignment week - 7
For a transport aircraft the maximum allowable load factor is 0.7. CDo = 0.02, AR = 10, e=0.9.
What is the maximum thrust loading ?
0.37
0.24 0.12 1.2
Accepted Answers:
0.37
At sea level for 40m/sec speed what will be the wing loading ? 105 N/m2
55 N/m2 20 N/m2 207 N/m2
Accepted Answers:
105 N/m2
For an aircraft having elliptical lift distribution with AR = 9.0 and CD0 =
0.02. For sustained turning at load factor of 6.0, which one of the following can be possible thrust loading ?
0.1 0.2 0.3 0.4
Accepted Answers:
0.4
29/12/2017 Aircraft Design - - Unit 8 - Week - 7
https://onlinecourses.nptel.ac.in/noc17_ae08/unit?unit=58&assessment=66 2/2
2 points 4)
2 points 5)
For an aircraft having elliptical lift distribution with AR = 9.0 and CD0 = 0.02. For sustained turning at load factor of 5.0, which one of the following can not be possible thrust loading ?
0.2 0.3 0.4 0.5
Accepted Answers:
0.2
1. For an aircraft CDo = 0.022, AR = 9.0, e = 0.8.
To achieve the climb angle of 10 deg, which one of the following can be a possible thrust loading?
0.1 0.14 0.2 0.25
Accepted Answers:
0.25
