INVESTIGATION OF FLOW-AROUND THE HEMISPHERICAL WING IN A GAS OUTERMOST FLOW


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Abstract

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.

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Исследование обтекания полусферического крыла в потоке газа, растекающегося от центра
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About the authors

I. S. Proteven

Siberian State Aerospace University named after academician M. F. Reshetnev

M. V. Kraev

Siberian State Aerospace University named after academician M. F. Reshetnev

Email: kayerfor@mail.ru

References

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  6. Wygnanski J., Fiedler H. E. Two-dimensional mixing region // Ibid. 1970. Vol. 41, pt. 2. P. 327-361.
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Copyright (c) 2013 Proteven I.S., Kraev M.V.

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