A Simple Method for Studying Aero-Propulsion Characteristics of a Distributed Electric Propulsion Aircraft

Author:

Yu Haoliang,Lei Tao,Mi Baigang,Zhang Xingyu,Zhang Xiaobin

Publisher

Springer Nature Singapore

Reference13 articles.

1. Yang, W., Fan, Z.L., Wu, W.H., et al.: Optimal design of distributed propeller layout considering slipstream effect. Acta Aerodyn. Sinica 39(3), 71−79 (2021). (in Chinese)

2. Zhang, T.J., Wei, C., et al.: Influence mechanism of propeller slipstream on wing of a distributed electric aircraft scheme. Acta Aeronaut. Astronaut. Sinica 42(S1), 726387 (2021). (in Chinese)

3. Zhiyong, C., Youxu, Y., Xingcui, Z., et al.: Rapid evaluation method for aerodynamic characteristics of distributed electric propulsion aircraft concept scheme. J. Beijing Univ. Aeronaut. Astronaut. (2022). (in Chinese)

4. Lei, Y., Yang, W.J., Huang, Y.Y.: Aerodynamic performance of distributed electric propulsion with wing interaction. J. Zhejiang Univ. Sci. A (Appl. Phys. Eng.) 23(1), 13 (2022)

5. Botero, E., Clarke, M.A., Erhard, R.M., Smart, J.T., Alonso, J.J., Blaufox, A.: Aerodynamic verification and validation of SUAVE. In: AIAA SCITECH 2022 Forum (2022)

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