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


Cite item

Full Text

Open Access Open Access
Restricted Access Access granted
Restricted Access Subscription Access

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

Supplementary files

Supplementary Files
Action
1. JATS XML

Copyright (c) 2016 Pleiades Publishing, Ltd.