INVESTIGATION OF TRANSONIC FLOW THROUGH LINEAR CASCADE WITH SINGLE BLADE INCIDENCE ANGLE OFFSET

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F22%3A00359031" target="_blank" >RIV/68407700:21220/22:00359031 - isvavai.cz</a>
Alternative codes found
RIV/61388998:_____/22:00583369
Result on the web
<a href="https://doi.org/10.14311/TPFM.2022.008" target="_blank" >https://doi.org/10.14311/TPFM.2022.008</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.14311/TPFM.2022.008" target="_blank" >10.14311/TPFM.2022.008</a>

Result language
angličtina
Original language name
INVESTIGATION OF TRANSONIC FLOW THROUGH LINEAR CASCADE WITH SINGLE BLADE INCIDENCE ANGLE OFFSET
Original language description
The contribution deals with numerical and experimental investigation of the effect of incidence angle offset in a two-dimensional section of a flat linear blade cascade in a high-speed wind tunnel. The aim of the work is to complement ongoing research of quasi-stationary approximation of aerodynamic flutter by examination of setups leading to transonic flow regimes. The numerical simulations were realized by finite-volume, in-house code developed on top of the open-source software package OpenFOAM. The experiments were conducted in correspondence with the setting of numerical simulations. The comparison of experimental and numerical data is presented on the isentropic Mach number distributions at various locations in the blade cascade. The description of transonic flow structures in the vicinity of blades is also provided.
Czech name
—
Czech description
—

Publication year
2022
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Similar results(10)