78475

Автор(ы): 

Вересников Г. С. (ИПУ РАН, Лаборатория 46)
Башкиров И. Г. (ИПУ РАН, Лаборатория 46)
Соболев Д. Н. (ИПУ РАН, Лаборатория 46)
Сапронов Д. Г. (ЦАГИ)

Автор(ов): 

4

Параметры публикации

Тип публикации: 

Доклад

Название: 

Algorithm for Computing the Parameters of a Low-Impact Sonic Boom Demonstrator Aircraft in Accordance with Specified Technical Requirements During Preliminary Aerodynamic Design Under Epistemic Uncertainty

ISBN/ISSN: 

979-8-3503-7571-8

DOI: 

10.1109/MLSD61779.2024.10739457

Наименование конференции: 

  • 2024 17th International Conference Management of large-scale system development (MLSD)

Наименование источника: 

  • Proceedings of the 17th International Conference Management of Large-Scale System Development (MLSD)

Город: 

  • Москва

Издательство: 

  • IEEE

Год издания: 

2024

Страницы: 

https://ieeexplore.ieee.org/document/10739457
Аннотация
An algorithm for calculating the aerodynamic layout and power plant parameters according to specified technical requirements (TR) at the stage of preliminary aerodynamic design (PAD) has been developed. A low-impact sonic boom demonstrator aircraft X-59 was chosen as a model. We use the uncertainty theory to account for non-deterministic data.

Библиографическая ссылка: 

Вересников Г.С., Башкиров И.Г., Соболев Д.Н., Сапронов Д.Г. Algorithm for Computing the Parameters of a Low-Impact Sonic Boom Demonstrator Aircraft in Accordance with Specified Technical Requirements During Preliminary Aerodynamic Design Under Epistemic Uncertainty / Proceedings of the 17th International Conference Management of Large-Scale System Development (MLSD). М.: IEEE, 2024. С. https://ieeexplore.ieee.org/document/10739457.