Journal of Civil Aviation University of China ›› 2021, Vol. 39 ›› Issue (2): 7-11.

• Civil Aviation • Previous Articles     Next Articles

Calculation of maximum failure speed of military aircraft 

ZHENG Fengmin, AN Y an    

  1. Xi'an Aircraft Design Institute of AV IC Xi爷an Aircraft Industry (Group) Company LTD, Xi爷an 710089, China
  • Received:2020-04-19 Revised:2020-04-19 Accepted:2020-03-09 Online:2021-04-10 Published:2021-11-27

Abstract: According to the calculation principle of failure speed, the aircraft motion simulation model is established. The key point is to combine the brake model, pneumatic model, engine model and landing gear system model, and to compile the calculation program to simulate the aircraft‘s acceleration run -off section and brake stop section. Taking one military aircraft as an example, a high-precision model solver based on the fourth-order Runge Kutta method is established, and the calculation method of the maximum failure speed of military aircraft is given. Calculation result of the algorithm can well fit the actual test flight data, providing reference for the actual training of troops.

Key words:  , maximum failure speed, simulation model, actual flight test 

CLC Number: