Volume 38 Issue 3
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HUANG Jingjie, ZHANG Xin, MENG Chao, et al. Effect of thrust reverser on the deceleration performance of civil aircraft[J]. Journal of Aerospace Power, 2023, 38(3):728-734 doi: 10.13224/j.cnki.jasp.20210215
Citation: HUANG Jingjie, ZHANG Xin, MENG Chao, et al. Effect of thrust reverser on the deceleration performance of civil aircraft[J]. Journal of Aerospace Power, 2023, 38(3):728-734 doi: 10.13224/j.cnki.jasp.20210215

Effect of thrust reverser on the deceleration performance of civil aircraft

doi: 10.13224/j.cnki.jasp.20210215
  • Received Date: 2021-05-07
    Available Online: 2023-02-10
  • The combined effect of the reverse thrust and weight increase of the thrust reverser on the deceleration performance of a civil aircraft was analyzed. A hypothetical turbofan model based on the CFM56 engine was established by Turbomatch software from Cranfield University, with A320 aircraft taken as the model. The propulsion system weight was estimated using the fan and turbine diameter. After discussion of aircraft deceleration benefit on the dry runway or icy runway, effects of the deflection angle and runway condition on the deceleration distance during conventional landing phase were analyzed. It showed that the thrust reversers were more efficient with small deflection angel. Based on a deflection angle of 55°, 10° reduction resulted in a deceleration benefit of approximately 7%. And the thrust reversers were more beneficial on the wet/icy runway, with the distance and time down by about 41% and 32% compared with the dry runway.

     

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