Aerodynamic/propulsion coupling model of vector electric propulsion systemChinese Full TextEnglish Full Text (MT)
XIA Jiyu;ZHOU Zhou;XU De;WANG Zhengping;School of Aeronautics, Northwestern Polytechnical University;
Abstract: This paper proposes an aerodynamic/propulsion coupling model to realize real-time and rapid evaluation of the aerodynamic and propulsion performance of the vector electric propulsion system by combining the theoretical model with the engineering experience model. To accurately describe the aerodynamic/propulsion coupling effect of the system, we first establish the propulsion model of the ducted fan by combining the propulsion enhancement coefficient formula and the engineering experience model.... More
Keywords:
electric propulsion system; aerodynamic/propulsion coupling; real-time calculation; electric ducted fan; lift enhancement of wing;
- Series:
(C) Architecture/ Energy/ Traffic/ Electromechanics, etc
- Subject:
Aeronautics and Astronautics Science and Engineering; Dynamical Engineering
- Classification Code:
V439.4
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