Discussion
In the Fourier solution of thin airfoil theory, the coefficient conventionally written as A zero depends on
Answer: C
The leading coefficient is the angle of attack less the mean of the camber-line slope taken over the chord. It is therefore the only coefficient that changes when the airfoil is rotated, and everything about how lift responds to incidence follows from it. Thickness plays no part anywhere in the theory.
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