V-shaped wings with an opening angle exceeding π at super- and hypersonic flow velocities
- Authors: Maksimov F.A.1, Ostapenko N.A.1
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Affiliations:
- Research Institute of Mechanics
- Issue: Vol 61, No 8 (2016)
- Pages: 412-417
- Section: Mechanics
- URL: https://journals.rcsi.science/1028-3358/article/view/190633
- DOI: https://doi.org/10.1134/S1028335816080139
- ID: 190633
Cite item
Abstract
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.
About the authors
F. A. Maksimov
Research Institute of Mechanics
Author for correspondence.
Email: f_a_maximov@mail.ru
Russian Federation, Moscow, 117192
N. A. Ostapenko
Research Institute of Mechanics
Email: f_a_maximov@mail.ru
Russian Federation, Moscow, 117192
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