Mechanical Engineering
Category
United states of America
Geographic Coverage
Not Available
Video URL
Not Available
Sale price (USD)
Not Available
Non-exclusive license price (USD)
Not Available
Exclusive license price (USD)
Not Available
Non-exclusive license royalty rate %
Availability
Patent family
Number of members in the patent family
Assignee(s) / Patent owner(s)
To see the additional information details please login and subscribe to a Premium account.

Stall prediction for aircraft

Patent Pending In fluid dynamics, a stall is a reduction in the lift coefficient generated by a foil as angle of attack increases.[1] This occurs when the critical angle of attack of the foil is exceeded. The critical angle of attack is typically about 15 degrees, but it may vary significantly depending on the fluid, foil, and Reynolds number.

BROKER APPLY submit an inquiry
photo To see the additional information details please login and subscribe to a Plus or Premium account.