Engineering Journal: Science and InnovationELECTRONIC SCIENCE AND ENGINEERING PUBLICATION
Certificate of Registration Media number Эл #ФС77-53688 of 17 April 2013. ISSN 2308-6033. DOI 10.18698/2308-6033
  • Русский
  • Английский
Article

On the issue of optimizing the supersonic business aircraft layout in order to reduce sonic boom

Published: 25.04.2022

Authors: Tyushina M.A., Tyushin A.V., Safin R.M.

Published in issue: #4(124)/2022

DOI: 10.18698/2308-6033-2022-4-2170

Category: Aviation and Rocket-Space Engineering | Chapter: Design, construction and production of aircraft

The paper focuses on reducing sonic boom by optimizing the aerodynamic configuration of the aircraft, as well as the forebody parameters. The study emphasizes the urgency of the problem of sonic boom generated by a supersonic business aircraft and introduces the database acquired from research into methods for reducing sonic boom, both as an individual problem and as part of multi-parameter optimization of a supersonic business aircraft. We systematized and processed the data and estimated the methods in terms of their influence, if applied, on the level of sonic boom. Furthermore, we matched each method to the aircraft design stages that are characteristic of its introduction into the configuration. This approach makes it possible to find layout solutions and assess them rapidly at the early stages of designing the configuration of this kind of aircraft.


References
[1] Biryuk V.I., Ibragimov M.R., Kovalenko V.V., Novikov A.P., Titov V.N., Chayka T.Yu., Chernavskikh IY.N., Yudin V.G. Uchenye zapiski TsAGI — TsAGI Science Journal, 2010, vol. 41, no. 5, pp. 1.
[2] Carlson H.W. The lower bound of attainable sonic-boom overpressure and design methods of approaching this limit. National Aeronautics and Space Administration, Technical Note D-1494, Washington, Oct., 1962.
[3] Sriram Rallabhandi. Sonic Boom Minimization through Vehicle Shape Optimization and Probabilistic Acoustic Propagation. Georgia Institute of Technology. ProQuest Dissertations Publishing, 2005, art. no. 3170096.
[4] Bratukhin A.G., Serebryansky S.A., Strelets D.Yu., et al. Tsifrovye tekhnologii v zhiznennom tsikle rossiyskoy konkurentosposobnoy aviatsionnoy tekhniki [Digital technologies in the life cycle of Russian competitive aviation equipment]. Moscow, MAI Publ., 2020, 448 p. ISBN 978-5-4316-0694-6
[5] Morgenstern J., Norstrud N. Final Report for the Advanced Concept Studies for Supersonic Commercial Transports Entering Service in the 2030 to 2035 Period. N+3 Supersonic Program, NASA/CR–2010-216796, no. PMF-01623.
[6] Ordaz I., Wintzer M., Rallabhandi S.K. full-carpet design of a low-boom demonstrator concept. In: 33rd AIAA Applied Aerodynamics Conference, AIAA AVIATION Forum, Dallas, TX, 2015, Paper no. 2261.
[7] Xuan H., Cheng S., Fang L. The Research of Supersonic Aircraft Low Sonic Boom Configuration Design and Optimizations. China Academy of Aerospace Aerodynamics, Yungang West Road, Beijing, 100074, P. R. China, 2016.
[8] Morgenstern J., Buonanno M. Advanced Concept Studies for Supersonic Commercial Transports Entering Service in the 2018-2020 Period Phase. NASA/CR–2015-218719, no. GRC-E-DAA-TN20996.
[9] Chernyshev S.L. Zvukovoy udar [Sonic boom]. TsAGI, Nauka Publ., 2011. ISBN 978-5-02-037961-9
[10] Barabanov A.V., Serebryansky S.A. Substantiation of choosing rational appearance of nose of aircraft with the use of mathematical modeling. A. V. S. A. Aerospace Systems, 2021, vol. 4, no. 2, pp. 171–177. DOI: 10.1007/s42401-020-00079-2
[11] Lengyan, Qian Zhansen. A CFD Based Sonic Boom Prediction Method and Investigation on the Parameters Affecting the Sonic Boom Signature. Aerodynamics Research Institute, Shenyang, 110034, China, 2014.