Отправить статью по E-mail Aerodynamic Design Method of Integrated Aircraft with Submerged Intake Devices and Power Plant Included into Airframe Carrying System
- Авторы: Kornev A.1, Sereda V.1, Migalin K.2
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Учреждения:
- Zhukovskii National Aerospace University “Kharkiv Aviation Institute”
- OOO HPF Rotor
- Выпуск: Том 61, № 1 (2018)
- Страницы: 14-22
- Раздел: Flight Vehicle Design
- URL: https://journals.rcsi.science/1068-7998/article/view/230382
- DOI: https://doi.org/10.3103/S1068799818010038
- ID: 230382
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Аннотация
This paper presents a theoretically and practically grounded architecture of design methods combination. A possibility and completeness of developing integral design solutions and intensifying the design process are provided by redistribution of emphases of numerical and natural experiments.
Об авторах
A. Kornev
Zhukovskii National Aerospace University “Kharkiv Aviation Institute”
Email: MigalinK@mail.ru
Украина, ul. Chkalova 17, Kharkiv, 61070
V. Sereda
Zhukovskii National Aerospace University “Kharkiv Aviation Institute”
Email: MigalinK@mail.ru
Украина, ul. Chkalova 17, Kharkiv, 61070
K. Migalin
OOO HPF Rotor
Автор, ответственный за переписку.
Email: MigalinK@mail.ru
Россия, ul. Rodiny 32, selo Podstepki, Stavropol’skii raion, Samara oblast, 445000
