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Address: Aviation Building,Youyi Campus, Northwestern Polytechnical University
Research on simulation Method of propeller power in the Model free-flight test
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Affiliation:

1.SChinese Flight Test Establishment,Yan Liang;2.CHINA AVIC INDUSTRY GENERAL AIRCRAFT INSTITUTE,Zhu-Hai

Clc Number:

V216.7

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    Abstract:

    That is necessary to simulate effects of propeller power, when the Aircraft with propeller is considered stall performance by scaled free-flight test. Combined with the analysis of simulate methods propeller power and criterion of dynamic similitude for modeling flight, and advanced the simulation method of propeller aircraft were investigated the stall, spin and recovery characteristics by free-flight test. Actual free-flight tests were performed to examine the method on four turbo-prop engines. The free-flight test results shows that the method real reflected the state of propeller power operation at the stall, the stall speed and stall characteristics were exactly obtained on influence of propeller power for full-size aircraft.

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ZHANG Jia-qi, WEI Biao, ZHANG Li-feng. Research on simulation Method of propeller power in the Model free-flight test[J]. Advances in Aeronautical Science and Engineering,2020,11(1):62-68

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History
  • Received:March 01,2019
  • Revised:June 22,2019
  • Adopted:July 01,2019
  • Online: February 23,2020
  • Published: