- #1
mengshuen
- 31
- 0
hello all,
i was reading up on aircraft design one fine day when they talked about landing speed; they have to be higher than one critical speed, the stalling speed.
if i remember correctly, is there another stalling speed, the upper limit? reynold's number increases at increasing speed of airflow, and the air would detach easily, lowering lift and causing turbulent airflow behind the trailing edge. am i correct?
i was reading up on aircraft design one fine day when they talked about landing speed; they have to be higher than one critical speed, the stalling speed.
if i remember correctly, is there another stalling speed, the upper limit? reynold's number increases at increasing speed of airflow, and the air would detach easily, lowering lift and causing turbulent airflow behind the trailing edge. am i correct?