Demonstration and validation flight test of scaled aircraft model and its key technologies

HE Kaifeng; MAO Zhongjun; WANG Qing; CHEN Hai

doi:10.7638/kqdlxxb-2017.0089

ACTA AERODYNAMICA SINICA > 2017 > 35(5): 671-679. > DOI: 10.7638/kqdlxxb-2017.0089

HE Kaifeng, MAO Zhongjun, WANG Qing, CHEN Hai. Demonstration and validation flight test of scaled aircraft model and its key technologies[J]. ACTA AERODYNAMICA SINICA, 2017, 35(5): 671-679. DOI: 10.7638/kqdlxxb-2017.0089

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Demonstration and validation flight test of scaled aircraft model and its key technologies

HE Kaifeng^{1, 2,},
MAO Zhongjun^2, ,,
WANG Qing^{1, 2},
CHEN Hai²

1.
State Key Laboratory of Aerodynamics, Mianyang 621000, China
2.
China Aerodynamics Research and Development Center, Mianyang 621000, China

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Received Date: May 16, 2017
Revised Date: September 19, 2017
Available Online: January 07, 2021

Graphical Abstract

Abstract

Abstract

Firstly, the flight tests and its application of scaled aircraft models at home and abroad are introduced in this paper. The study topics are summarized as follows:the demonstration and validation of aerodynamic configurations, the flight test of aerodynamic forces, the flight test of dangerous boundaries, as well as the demonstration and validation test with new concepts and technologies. Secondly, this paper analyzes the key technologies of model flight test such as powered flight with autonomous control, quick model structure design and manufacture, model power system design and test, flight controller design and test, high precision measurement, and aerodynamic coefficients identification. Some results of CARDC (China Aerodynamics Research and Development Center) research on these key technologies are shown. Finally, the potential development directions of model flight test are prospected.
- scaled model flight test,
- aerodynamic research,
- aerodynamic coefficients identification,
- demonstration and validation

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References (23)

References

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