This paper deals with in-flight simulation of the behaviour of two longitudinal oscillations that occured on JJ-7 aircraft by using BW-1 variable stability aircraft.

 
  • 本文論述了BW-1變穩機空中飛行模擬H-7飛機發(fā)生兩次縱向擺動(dòng)時(shí)飛行狀態(tài)特性,通過(guò)試飛研究其飛行品質(zhì),校核駕駛員誘發(fā)振蕩(PIO)發(fā)生的可能性;
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