All

What are you looking for?

All
Projects
Results
Organizations

Quick search

  • Projects supported by TA ČR
  • Excellent projects
  • Projects with the highest public support
  • Current projects

Smart search

  • That is how I find a specific +word
  • That is how I leave the -word out of the results
  • “That is how I can find the whole phrase”

Analysis of Synthetic Jet Flow by Means of Proper Orthogonal Decomposition and Dynamic Mode Decomposition Based on CFD Data

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F15%3A00242221" target="_blank" >RIV/68407700:21220/15:00242221 - isvavai.cz</a>

  • Result on the web

  • DOI - Digital Object Identifier

Alternative languages

  • Result language

    angličtina

  • Original language name

    Analysis of Synthetic Jet Flow by Means of Proper Orthogonal Decomposition and Dynamic Mode Decomposition Based on CFD Data

  • Original language description

    The results of numerical simulation of synthetic jet flow are analysed by means of modal decomposition technique. Three typical laminar regimes are compared from the point of view of modal decomposition. The first regime is without synthetic jet creationwith Reynolds number Re = 76 and Stokes number S = 19:7. The regime of synthetic jet without vortex roll-up is defined by Re = 145 and S = 19.7. The third regime of synthetic jet with vortex roll-up is regime with Re = 329 and S = 19.7. Modal decomposition of obtained flow fields is done using proper orthogonal decomposition (POD) and using dynamic mode decomposition (DMD). Vortex street like structure with travelling vortex ring is identified using the topology of dynamic modes where the vortexes arevisualized using the concept of residual vorticity. The speed of travelling vortex is evaluated using the wavelength identified from DMD modes.

  • Czech name

  • Czech description

Classification

  • Type

    O - Miscellaneous

  • CEP classification

    JU - Aeronautics, aerodynamics, aeroplanes

  • OECD FORD branch

Result continuities

  • Project

    <a href="/en/project/GA14-08888S" target="_blank" >GA14-08888S: Control of flow fields by means of fluid oscillation</a><br>

  • Continuities

    P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Others

  • Publication year

    2015

  • Confidentiality

    S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů