Discussion
A wing aerodynamic centre lies at 0.25 chord and the centre of gravity at 0.32. The wing's own contribution to the moment slope is
Answer: A
The contribution is the centre of gravity position less the aerodynamic centre position, \( 0.32 - 0.25 = 0.07 \), and a positive value is destabilising. Only the tailplane's negative contribution can then make the whole aeroplane stable.
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