Aerodynamic Design Method of Integrated Aircraft with Submerged Intake Devices and Power Plant Included into Airframe Carrying System
- 作者: Kornev A.1, Sereda V.1, Migalin K.2
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隶属关系:
- Zhukovskii National Aerospace University “Kharkiv Aviation Institute”
- OOO HPF Rotor
- 期: 卷 61, 编号 1 (2018)
- 页面: 14-22
- 栏目: Flight Vehicle Design
- URL: https://journals.rcsi.science/1068-7998/article/view/230382
- DOI: https://doi.org/10.3103/S1068799818010038
- ID: 230382
如何引用文章
详细
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.
作者简介
A. Kornev
Zhukovskii National Aerospace University “Kharkiv Aviation Institute”
Email: MigalinK@mail.ru
乌克兰, ul. Chkalova 17, Kharkiv, 61070
V. Sereda
Zhukovskii National Aerospace University “Kharkiv Aviation Institute”
Email: MigalinK@mail.ru
乌克兰, ul. Chkalova 17, Kharkiv, 61070
K. Migalin
OOO HPF Rotor
编辑信件的主要联系方式.
Email: MigalinK@mail.ru
俄罗斯联邦, ul. Rodiny 32, selo Podstepki, Stavropol’skii raion, Samara oblast, 445000