MODEL RESEARCH TECHNOLOGIES FOR CREATING THE PERFORATED DESIGN OF THE SHEATHER EQUIPMENT
Roman Nikolaevich (N) Aliafanov
Abstract
The article deals with modern aspects of the use of a perforated casing design with combined holes and a damping cavity. The main emphasis of the research is made on the field of their application and control of the laminar-turbulent transition near aerodynamic surfaces of aircraft with a perforated surface with holes of various geometric configurations, including with combined geometric shapes that have blind damping cavities