V-shaped wings with an opening angle exceeding π at super- and hypersonic flow velocities


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The results of theoretical investigation of an ideal-gas asymmetrical flow around V-shaped wings with an opening angle exceeding π and having supersonic forward edges at all modes are presented.

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F. Maksimov

Research Institute of Mechanics

编辑信件的主要联系方式.
Email: f_a_maximov@mail.ru
俄罗斯联邦, Moscow, 117192

N. Ostapenko

Research Institute of Mechanics

Email: f_a_maximov@mail.ru
俄罗斯联邦, Moscow, 117192

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