Discussion
A wing's leading edge is described as subsonic when
Answer: B
What matters is the velocity component normal to the leading edge. If the edge is swept far enough to lie inside the Mach cone, that component is below sonic speed and the edge behaves in a subsonic manner, permitting a rounded nose and leading-edge suction even though the aircraft is supersonic.
No comment is present. Be the first to comment.
Loading…
Post your comment
Please log in or register to post a comment.
Examination Categories
- SSC Exams
- Banking Exams
- Teaching Exams
- Civil Services Exams
- Railways Exams
- Engineering Recruitment Exams
- Defence Exams
- State Government Exams
- Police Exams
- Insurance Exams
- Nursing Exams
- Other Government Exams
- NRA CET
- PG Entrance Exams
- Campus Placement
- MBA Entrance Exams
- CUET and UG Entrance
- Judiciary Exams
- Regulatory Body Exams
- Software Development