Design and aerodynamic analysis of the morphing waverider with rotating telescopic wing for wide-speed-range flight
•A novel morphing waverider with rotating telescopic wings is proposed for wide-speed-range flight.•The vehicle's configuration supports clustered launch deployment and runway landing capabilities.•Multi-objective optimization achieves a balance between volumetric efficiency, L/D ratio, and win...
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| Veröffentlicht in: | Aerospace science and technology Jg. 158; S. 109941 |
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| Format: | Journal Article |
| Sprache: | Englisch |
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Elsevier Masson SAS
01.03.2025
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| ISSN: | 1270-9638 |
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| Abstract | •A novel morphing waverider with rotating telescopic wings is proposed for wide-speed-range flight.•The vehicle's configuration supports clustered launch deployment and runway landing capabilities.•Multi-objective optimization achieves a balance between volumetric efficiency, L/D ratio, and wing area.•A rear fairing design significantly improves aerodynamic performance in subsonic regime.•The fuselage contributes 49.5 % of total lift at high angles of attack, enhancing stall resistance.
Wide-speed-range vehicles represent a burgeoning research area in aerospace, challenged by the conflicting aerodynamic demands of different flight regimes. This study proposes a novel "waverider with rotating telescopic wing" configuration for clustered launch deployments, capable of morphing to meet both hypersonic and subsonic flight requirements. The research focuses on two key aspects: firstly, presenting a morphing vehicle design for wide-speed-range flight; and secondly, developing a multi-objective optimization method for the waverider fuselage subject to multiple constraints, followed by a detailed analysis of the design results. Performance analysis under various flight conditions revealed that rear surface drag significantly hinders subsonic performance. To address this, the study investigates the design and impact of a rear fairing across different speeds. Results demonstrate that the rear fairing effectively enhances aerodynamic performance in both hypersonic and subsonic regimes. This promising configuration addresses the challenges of wide-speed-range flight while enabling cost-effective clustered launches. When coupled with reusable launch vehicles, it unlocks significant potential for applications such as rapid intercontinental transportation. |
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| AbstractList | •A novel morphing waverider with rotating telescopic wings is proposed for wide-speed-range flight.•The vehicle's configuration supports clustered launch deployment and runway landing capabilities.•Multi-objective optimization achieves a balance between volumetric efficiency, L/D ratio, and wing area.•A rear fairing design significantly improves aerodynamic performance in subsonic regime.•The fuselage contributes 49.5 % of total lift at high angles of attack, enhancing stall resistance.
Wide-speed-range vehicles represent a burgeoning research area in aerospace, challenged by the conflicting aerodynamic demands of different flight regimes. This study proposes a novel "waverider with rotating telescopic wing" configuration for clustered launch deployments, capable of morphing to meet both hypersonic and subsonic flight requirements. The research focuses on two key aspects: firstly, presenting a morphing vehicle design for wide-speed-range flight; and secondly, developing a multi-objective optimization method for the waverider fuselage subject to multiple constraints, followed by a detailed analysis of the design results. Performance analysis under various flight conditions revealed that rear surface drag significantly hinders subsonic performance. To address this, the study investigates the design and impact of a rear fairing across different speeds. Results demonstrate that the rear fairing effectively enhances aerodynamic performance in both hypersonic and subsonic regimes. This promising configuration addresses the challenges of wide-speed-range flight while enabling cost-effective clustered launches. When coupled with reusable launch vehicles, it unlocks significant potential for applications such as rapid intercontinental transportation. |
| ArticleNumber | 109941 |
| Author | Zhang, Ligang Jing, Biao Qiao, Nanxuan Ma, Tielin Fu, Jingcheng |
| Author_xml | – sequence: 1 givenname: Nanxuan surname: Qiao fullname: Qiao, Nanxuan organization: School of Aeronautic Science and Engineering, Beihang University, Beijing 100191, PR China – sequence: 2 givenname: Tielin surname: Ma fullname: Ma, Tielin organization: Institute of Unmanned System, Beihang University, Beijing 100191, PR China – sequence: 3 givenname: Biao surname: Jing fullname: Jing, Biao organization: School of Aeronautic Science and Engineering, Beihang University, Beijing 100191, PR China – sequence: 4 givenname: Jingcheng orcidid: 0000-0002-8430-601X surname: Fu fullname: Fu, Jingcheng organization: Institute of Unmanned System, Beihang University, Beijing 100191, PR China – sequence: 5 givenname: Ligang surname: Zhang fullname: Zhang, Ligang email: 08985@buaa.edu.cn organization: Institute of Unmanned System, Beihang University, Beijing 100191, PR China |
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| Keywords | Morphing aircraft Aerodynamic performance Multi-object optimization Wide-speed-range vehicle Rotating telescoping wing |
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