

MCQOPTIONS
Saved Bookmarks
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. |
When velocity potential (ϕ) exits, the flow is _________ |
A. | rotational |
B. | irrotational |
C. | laminar |
D. | turbulent |
Answer» C. laminar | |
2. |
In the source flow, the tangential velocity component is _________ |
A. | 0 |
B. | 1 |
C. | not defined |
D. | infinity |
Answer» B. 1 | |