Enviar artigo por via de e-mail INVESTIGATION OF FLOW-AROUND THE HEMISPHERICAL WING IN A GAS OUTERMOST FLOW
- Autores: Proteven I.S.1, Kraev M.V.1
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Afiliações:
- Siberian State Aerospace University named after academician M. F. Reshetnev
- Edição: Volume 14, Nº 2 (2013)
- Páginas: 137-139
- Seção: Articles
- URL: https://journals.eco-vector.com/2712-8970/article/view/503764
- ID: 503764
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Resumo
On the basis of the model of radial gas flow-around the hemispherical surface the authors substantiate the ability to create enough lifting fore for the aircraft of an unconventional shape. During the analysis of possible design solutions the authors detected the optimal geometry of the wing and the propulsion system and peformed experimental researches on estimation of the lifting force.
Palavras-chave
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Исследование обтекания полусферического крыла в потоке газа, растекающегося от центра×
Sobre autores
I. Proteven
Siberian State Aerospace University named after academician M. F. Reshetnev
M. Kraev
Siberian State Aerospace University named after academician M. F. Reshetnev
Email: kayerfor@mail.ru
Bibliografia
- Лойцянский Л. Г. Механика жидкости и газа. М. : Наука, 1978.
- Шлихтинг Г. Теория пограничного слоя. М. : Наука, 1974.
- Абрамович Г. Н. Теория турбулентных струй. М. : Физматгиз, 1960.
- Гиневский А. С. Теория турбулентных струй и следов. М. : Машиностроение, 1969.
- Bradbury L. J. S. The structure of a self-preserving turbulent plane jet. // J. Fluid Mech. 1965. Vol. 23, pt. 1. Р. 31-64.
- Wygnanski J., Fiedler H. E. Two-dimensional mixing region // Ibid. 1970. Vol. 41, pt. 2. P. 327-361.
- Баренблатт Г. И. Подобие, автомодельность, промежуточная асимптотика. Л. : Гидрометеоиздат, 1982.
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