Bi-layer sizing and design optimization method of propulsion system for electric vertical takeoff and landing aircraft
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DOI: 10.1016/j.energy.2023.129052
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References listed on IDEAS
- Zhang, Jinning & Roumeliotis, Ioannis & Zolotas, Argyrios, 2022. "Model-based fully coupled propulsion-aerodynamics optimization for hybrid electric aircraft energy management strategy," Energy, Elsevier, vol. 245(C).
- Bravo, Guillem Moreno & Praliyev, Nurgeldy & Veress, Árpád, 2021. "Performance analysis of hybrid electric and distributed propulsion system applied on a light aircraft," Energy, Elsevier, vol. 214(C).
- Rohacs, Jozsef & Rohacs, Daniel, 2020. "Energy coefficients for comparison of aircraft supported by different propulsion systems," Energy, Elsevier, vol. 191(C).
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Cited by:
- Luo, Qiaodan & Zhao, Shengfeng & Zhou, Shiji & Yao, Lipan & Yang, Chengwu & Lu, Xingen & Zhu, Junqiang, 2024. "Influence of diversified dihedral stator on the thermodynamic performance and flow loss characteristics of a variable core driven fan stage," Energy, Elsevier, vol. 294(C).
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Keywords
Aircraft design; Optimization; Vertical takeoff and landing; Electric propulsion;All these keywords.
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