Email this article Aerodynamic Design Method of Integrated Aircraft with Submerged Intake Devices and Power Plant Included into Airframe Carrying System
- Authors: Kornev A.V.1, Sereda V.A.1, Migalin K.V.2
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Affiliations:
- Zhukovskii National Aerospace University “Kharkiv Aviation Institute”
- OOO HPF Rotor
- Issue: Vol 61, No 1 (2018)
- Pages: 14-22
- Section: 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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Abstract
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.
About the authors
A. V. Kornev
Zhukovskii National Aerospace University “Kharkiv Aviation Institute”
Email: MigalinK@mail.ru
Ukraine, ul. Chkalova 17, Kharkiv, 61070
V. A. Sereda
Zhukovskii National Aerospace University “Kharkiv Aviation Institute”
Email: MigalinK@mail.ru
Ukraine, ul. Chkalova 17, Kharkiv, 61070
K. V. Migalin
OOO HPF Rotor
Author for correspondence.
Email: MigalinK@mail.ru
Russian Federation, ul. Rodiny 32, selo Podstepki, Stavropol’skii raion, Samara oblast, 445000
