Мақаланы E-mail арқылы жіберу Aerodynamic Design Method of Integrated Aircraft with Submerged Intake Devices and Power Plant Included into Airframe Carrying System
- Авторлар: Kornev A.V.1, Sereda V.A.1, Migalin K.V.2
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Мекемелер:
- Zhukovskii National Aerospace University “Kharkiv Aviation Institute”
- OOO HPF Rotor
- Шығарылым: Том 61, № 1 (2018)
- Беттер: 14-22
- Бөлім: Flight Vehicle Design
- URL: https://journals.rcsi.science/1068-7998/article/view/230382
- DOI: https://doi.org/10.3103/S1068799818010038
- ID: 230382
Дәйексөз келтіру
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Рұқсат берілді
Тек жазылушылар үшін
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.
Авторлар туралы
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
Хат алмасуға жауапты Автор.
Email: MigalinK@mail.ru
Ресей, ul. Rodiny 32, selo Podstepki, Stavropol’skii raion, Samara oblast, 445000
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