Discussion
Which effect makes the derivatives of a large transport differ between a rigid model and the real aeroplane at high dynamic pressure?
Answer: C
Aeroelastic deformation is the effect in question: under load the wing and tail twist in a direction that reduces the incidence change they achieve, so the real derivatives are softer than the rigid ones and the shortfall grows with dynamic pressure. Density is already accounted for by the dynamic pressure in the conversion. Reynolds number matters, especially near the stall, but it is a separate correction. Landing gear is a configuration change rather than a rigid-to-flexible one.
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