Bypass Boundary Layer Transition on Flat Plate by Adverse Pressure Gradient

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F61388998%3A_____%2F19%3A00518115" target="_blank" >RIV/61388998:_____/19:00518115 - isvavai.cz</a>
Result on the web
<a href="https://www.epj-conferences.org/articles/epjconf/pdf/2019/18/epjconf_efm18_02077.pdf" target="_blank" >https://www.epj-conferences.org/articles/epjconf/pdf/2019/18/epjconf_efm18_02077.pdf</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1051/epjconf/201921302077" target="_blank" >10.1051/epjconf/201921302077</a>

Result language
angličtina
Original language name
Bypass Boundary Layer Transition on Flat Plate by Adverse Pressure Gradient
Original language description
Bypass boundary layer transition in flows on flat plate by adverse pressure gradient was investigated experimentally. It was measuered cases with combination of adverse pressure gradient by different free stream turbulence intenzity. Hot wire anemometry technique was used. Measuerement were made on flat plate in closed wind tunnel. Adverse pressure gradient was set by diffuser in tested section of wind tunnel. Grid turbulence of free stream was controlled by screen. Hot wire anemometry technique was used, intermitency factor was evaluated. Results were compared wih cases with simpliest conditions.
Czech name
—
Czech description
—

Project
<a href="/en/project/GA17-01088S" target="_blank" >GA17-01088S: 3D Instability of a Shear Layer in Adverse Pressure Gradient</a><br>
Continuities
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year
2019
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Similar results(10)