asymmetric blade effect मीनिंग इन हिंदी

The asymmetric blade effect is dependent on thrust, and is proportional to forward velocity ( specifically CAS ) and, while generally insignificant during the initial ground roll for tail-wheel aircraft, will give a pronounced nose-left tendency during the later stages of the ground roll, particularly if the thrust axis is kept inclined to the flight path vector ( i . e . tail-wheel in contact with runway ).