Flight Test of Stalling Speed for ChangGong-91

창공-91 실속속도 비행시험

  • 이정훈 (한국항공우주연구원 항공사업단) ;
  • 김칠영 (한국항공대학교 항공운항학과)
  • Published : 2008.09.30

Abstract

The stalling speed flight test of light airplane, ChangGong-91, was performed to acquire the certification. With power-off engine condition, the wings level stall flight tests were conducted at the aircraft configuration of various flap angle - clean, 20degree, and full flap, respectively. They were performed considering with the combination of the maximum and minimum test weight, and forward and afterward center of gravity. The stalling speeds and the minimum speeds of light airplane were determined from the results of flight test. Also, the appropriateness of stall warning speeds are evaluated through the flight test measures. The airplane is recoverable only with pitch control and engine throttle from stall state without exceptional operation.

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