Explore topic-wise MCQs in Aerodynamics Questions and Answers.

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

1.	Given an angle of attack 5° and c = 5m, the moment coefficient about the leading edge is_____
A.	-0.137
B.	-0.685
C.	-7.8
D.	-0.27
Answer» B. -0.685

Discussion

2.	The Kutta condition is not satisfied at the trailing edge where θ=π in transformed coordinates for a symmetrical airfoil.
A.	True
B.	False
Answer» C.

Discussion

Explore topic-wise MCQs in Aerodynamics Questions and Answers.

Given an angle of attack 5° and c = 5m, the moment coefficient about the leading edge is_____

The Kutta condition is not satisfied at the trailing edge where θ=π in transformed coordinates for a symmetrical airfoil.