61 to 70 of 104 Results
Gzip Archive - 37.2 GB -
MD5: 71a5cd5e0524e0ba01bf3ca039e265f1
Simulation results of OpenFOAM & MBDyn for a flying cycloidal rotor |
Gzip Archive - 26.1 GB -
MD5: dfbf15f4f36da29bb5a366272b286102
Simulation results of OpenFOAM & MBDyn for a flying cycloidal rotor, without a coupling of the blade deformation |
Gzip Archive - 3.6 KB -
MD5: 26b1528e385b1b7f1bc9d62bef666387
Custom OpenFOAM class to couple a rotation motion via preCICE with OpenFOAM. |
Adobe PDF - 76.3 KB -
MD5: e1213e81aaf62355f382d855538c4369
README |
Gzip Archive - 5.6 MB -
MD5: a05ab0ca6832cf0848502d2481f7b6fb
Install guide |
Gzip Archive - 5.3 KB -
MD5: 21baee31bc807196bafe2cecbd5f9920
Custom OpenFOAM class to simulate multiple deforming bodies on a chimera background mesh.
Copyright (c): Louis Gagnon |
Oct 21, 2021
Huang, Doudou; Gagnon, Louis, 2021, "Data for: Relying on Dynamically Morphing Blades to Increase the Efficiency of a Cycloidal Rotor", https://doi.org/10.18419/DARUS-2191, DaRUS, V1
OpenFOAM simulation case files and results accompanying the article having the same title are included. The pressure, velocity and vorticity fields could be visualized by using Paraview. The simulation of the last rotor revolution of each case can be reproduced by running the restartLastCycle.sh script. The supplementary cases which are not documen... |
Oct 21, 2021 -
Data for: Relying on Dynamically Morphing Blades to Increase the Efficiency of a Cycloidal Rotor
Bzip Archive - 1.5 GB -
MD5: 9b0d387893119e3ca26666b5951ac096
OpenFOAM simulation results: symmetric leading edge camber of 4% at position p = 0.1 |
Oct 21, 2021 -
Data for: Relying on Dynamically Morphing Blades to Increase the Efficiency of a Cycloidal Rotor
Bzip Archive - 1.8 GB -
MD5: bc41c94349ca03d9b2b6c99e953486ae
OpenFOAM simulation results: symmetric leading edge camber of 2% at position p = 0.3 |
Oct 21, 2021 -
Data for: Relying on Dynamically Morphing Blades to Increase the Efficiency of a Cycloidal Rotor
Bzip Archive - 1.6 GB -
MD5: e7b1db39ed8d272ce6c1636c22f657fd
OpenFOAM simulation results: asymmetric leading edge camber with 2% camber at top and 6% camber at bottom, p=0.3 |