- Issue
- Journal of Siberian Federal University. Engineering & Technologies. 2018 11 (2)
- Authors
- Alifanov, Roman N.; Starodubtsev, Pavel A.
- Contact information
- Alifanov, Roman N.: Far Eastern State Technical Fisheries University Maritime Institute 52V Lugovaya, Vladivostok Str., 690078, Russia; Starodubtsev, Pavel A.: Far Eastern State Technical Fisheries University Maritime Institute 52V Lugovaya, Vladivostok Str., 690078, Russia;
- Keywords
- aircraft; combined perforations; damping cavity; boundary layer; frictional resistance; perforated surface
- 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
- Pages
- 198-212
- Paper at repository of SibFU
- https://elib.sfu-kras.ru/handle/2311/70962
This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License (CC BY-NC 4.0).