Volume 39 Issue 11
Nov.  2013
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Jiang Qideng. Flight test of high sink speed symmetric landing used in land-based aircraft strength verification[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(11): 1421-1425. (in Chinese)
Citation: Jiang Qideng. Flight test of high sink speed symmetric landing used in land-based aircraft strength verification[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(11): 1421-1425. (in Chinese)

Flight test of high sink speed symmetric landing used in land-based aircraft strength verification

  • Received Date: 04 Jan 2013
  • Publish Date: 30 Nov 2013
  • High sink speed landing was discussed which was used to verify the strength and rigidity and shock-absorbing ability of landing gear in land-based airplane flight test. Sink speed was one of the key factors in landing gear design and verification. In fact, aircraft landing was effected by many factors, so it is very difficult and full of high risk for pilot to manipulate an aircraft to land at sink speed regulated by specifications. Landing and touchdown methods,such as floating-drop and direct-gliding and landing training were put forward and used in flight tests. According to this, the sink rate of a land-based airplane flight test in domestic reached 2.47m/s, which is the maximum up to now.So the landing gears of this type aircraft satisfy relevant specifications.

     

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