Research progress of aerodynamic configuration technology of low sonic boom supersonic aircraft
The aerodynamic configuration of supersonic aircraft has an important effect on the intensity of sonic boom, and the low sonic boom supersonic configuration is the key of the new generation supersonic aircraft, so the aerodynamic configuration of low sonic boom supersonic aircraft is researched exte...
| Main Authors: | , , , , , |
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| Format: | Article |
| Language: | zho |
| Published: |
Editorial Department of Advances in Aeronautical Science and Engineering
2023-08-01
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| Series: | Hangkong gongcheng jinzhan |
| Subjects: | |
| Online Access: | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2022101?st=article_issue |
| _version_ | 1797682284608880640 |
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| author | SU Fengnian ZHONG Ping ZENG Hui LUO Yuepei CHEN Xilan GUO Chuwei |
| author_facet | SU Fengnian ZHONG Ping ZENG Hui LUO Yuepei CHEN Xilan GUO Chuwei |
| author_sort | SU Fengnian |
| collection | DOAJ |
| description | The aerodynamic configuration of supersonic aircraft has an important effect on the intensity of sonic boom, and the low sonic boom supersonic configuration is the key of the new generation supersonic aircraft, so the aerodynamic configuration of low sonic boom supersonic aircraft is researched extensively. Based on the systematic investigation of foreign sonic boom suppression technologies, six main aerodynamic methods of foreign low sonic boom supersonic aircraft are introduced, including aircraft volume and lift distribution optimization, wing sweep angle change, wing dihedral angle utilization, slender fuselage and wave suppression cone usage, and engine installed on the wing. Four main aerodynamic configuration types of low boom supersonic aircraft are summarized and analyzed. According to the aerodynamic configurations of current supersonic aircraft, it is concluded that the delta configuration is the mainstream aerodynamic configuration of the next generation environmentally friendly aircraft. The development trend of the aerodynamic configuration technologies of low boom supersonic aircraft is prospected. |
| first_indexed | 2024-03-11T23:57:30Z |
| format | Article |
| id | doaj.art-bae22d07f6c744bbadd6c707916413f3 |
| institution | Directory Open Access Journal |
| issn | 1674-8190 |
| language | zho |
| last_indexed | 2024-03-11T23:57:30Z |
| publishDate | 2023-08-01 |
| publisher | Editorial Department of Advances in Aeronautical Science and Engineering |
| record_format | Article |
| series | Hangkong gongcheng jinzhan |
| spelling | doaj.art-bae22d07f6c744bbadd6c707916413f32023-09-18T07:34:35ZzhoEditorial Department of Advances in Aeronautical Science and EngineeringHangkong gongcheng jinzhan1674-81902023-08-01144183010.16615/j.cnki.1674-8190.2023.04.0220230402Research progress of aerodynamic configuration technology of low sonic boom supersonic aircraftSU Fengnian0ZHONG Ping1ZENG Hui2LUO Yuepei3CHEN Xilan4GUO Chuwei5Computational Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 621000, ChinaComputational Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 621000, ChinaComputational Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 621000, ChinaComputational Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 621000, ChinaComputational Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 621000, ChinaComputational Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 621000, ChinaThe aerodynamic configuration of supersonic aircraft has an important effect on the intensity of sonic boom, and the low sonic boom supersonic configuration is the key of the new generation supersonic aircraft, so the aerodynamic configuration of low sonic boom supersonic aircraft is researched extensively. Based on the systematic investigation of foreign sonic boom suppression technologies, six main aerodynamic methods of foreign low sonic boom supersonic aircraft are introduced, including aircraft volume and lift distribution optimization, wing sweep angle change, wing dihedral angle utilization, slender fuselage and wave suppression cone usage, and engine installed on the wing. Four main aerodynamic configuration types of low boom supersonic aircraft are summarized and analyzed. According to the aerodynamic configurations of current supersonic aircraft, it is concluded that the delta configuration is the mainstream aerodynamic configuration of the next generation environmentally friendly aircraft. The development trend of the aerodynamic configuration technologies of low boom supersonic aircraft is prospected.http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2022101?st=article_issuesupersonic aircraftlow sonic boomaerodynamic configurationsonic boom suppression technology |
| spellingShingle | SU Fengnian ZHONG Ping ZENG Hui LUO Yuepei CHEN Xilan GUO Chuwei Research progress of aerodynamic configuration technology of low sonic boom supersonic aircraft Hangkong gongcheng jinzhan supersonic aircraft low sonic boom aerodynamic configuration sonic boom suppression technology |
| title | Research progress of aerodynamic configuration technology of low sonic boom supersonic aircraft |
| title_full | Research progress of aerodynamic configuration technology of low sonic boom supersonic aircraft |
| title_fullStr | Research progress of aerodynamic configuration technology of low sonic boom supersonic aircraft |
| title_full_unstemmed | Research progress of aerodynamic configuration technology of low sonic boom supersonic aircraft |
| title_short | Research progress of aerodynamic configuration technology of low sonic boom supersonic aircraft |
| title_sort | research progress of aerodynamic configuration technology of low sonic boom supersonic aircraft |
| topic | supersonic aircraft low sonic boom aerodynamic configuration sonic boom suppression technology |
| url | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2022101?st=article_issue |
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