Explore topic-wise MCQs in Aircraft Design Questions and Answers.

This section includes 2 Mcqs, each offering curated multiple-choice questions to sharpen your Aircraft Design Questions and Answers knowledge and support exam preparation. Choose a topic below to get started.

1.	Determine the value of drag at which we can have minimum power if given reference area is 10m2 and zero lift drag coefficient is 0.5. Consider q as 120Pa.
A.	2400N
B.	1.25
C.	9.85
D.	4500 KN
Answer» B. 1.25

Discussion

2.	Following diagram represents _________
A.	lift induced thrust required
B.	zero lift thrust required
C.	drag polar
D.	lift curve
Answer» B. zero lift thrust required

Discussion

Explore topic-wise MCQs in Aircraft Design Questions and Answers.

Determine the value of drag at which we can have minimum power if given reference area is 10m2 and zero lift drag coefficient is 0.5. Consider q as 120Pa.

Following diagram represents _________