Stall (flight)

Stall (flight)

Jesse Russell Ronald Cohn

     

бумажная книга



ISBN: 978-5-5092-6162-6

High Quality Content by WIKIPEDIA articles! In fluid dynamics, a stall is a reduction in the lift coefficient generated by a foil as angle of attack increases. 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.