In this article, the growth of aerodynamic efficiency and the growth of the wing structural
stress is studied for DLR-F4 typical transport aircraft wing-body, after installing classical …

The paper presents aerodynamic characteristics of thin cylindrical and conical shells in the
incompressible flow. Experimental data and results of numerical simulation in the …

The optimization of the aerodynamic load distribution (circulation G) has been performed
along the span of the complex lifting system, which provides the minimum induced drag …

The paper considers the problem of high-velocity flow past a perfectly sharp edge. The
solution was carried out using the model kinetic equation for polyatomic gases and the …

The article explores the possibility of improving the aerodynamic properties of a supercritical-
airfoil wing, typical for a modern passenger aircraft, using delta planform passive devices of …

The results of flow field numerical simulation on the typical wing-body prototype of the
modern DLR-F4 airliner under sub-and transonic compressible air flow are presented. Using …

В статье изучена возможность улучшения аэродинамических характеристик типичного
крыла пассажирского самолета со сверхкритическим профилем с помощью пассивных …

The results are given on the experimental studies of integral aerodynamic characteristics of
X-47B-type “flying wing” unmanned aerial vehicle model. The dependence of the lift …