Authors | A.M. Pavlyuchenko, O.M. Shyiko |
Affiliations |
Sumy National Agricultural University, 160, G. Kondratyeva Str., 40021 Sumy, Ukraine |
Е-mail | |
Issue | Volume 10, Year 2018, Number 5 |
Dates | Received 28 July 2018; revised manuscript received 22 October 2018; published online 29 October 2018 |
Citation | A.M. Pavlyuchenko, O.M. Shyiko, J. Nano- Electron. Phys. 10 No 5, 05019 (2018) |
DOI | https://doi.org/10.21272/jnep.10(5).05019 |
PACS Number(s) | 47.85.Gj |
Keywords | Turbulent supersonic boundary layer, Porous plate, Air injection, Heating (7) , Nonisothermicity, Ther-mal radiation, СO2-laser. |
Annotation |
A method for investigating the structure in a nonisothermal turbulent boundary layer of a streamlined flat porous surface in a supersonic wind tunnel with the use of thermal radiation from a CO2-laser was developed to create a heat flux on this surface. The velocity profiles on the porous plate are measured with air blowing and non-isothermicity. The use of CO2-laser radiation in an aerophysical experiment opens up the possibility of studying the thermal protection of a surface by means of porous injection of gases and on ablating surfaces, the study of heat transfer by convection and heat radiation when injected through a porous surface of optically active gases (CO2, SF6, etc.). |
List of References English version of article |