Workshop for integrated propeller prediction (WIPP)
Using the tip-mounted propeller geometry from the WIPP project as the baseline of the numerical investigation of novel rotorcraft propulsion systems, the method used in the HMB3 solver was validated against experimental data.
Airframe design analysis |
Lift changes brought by wing anhedral/dihedral angles |
This work is ongoing and more high-fidelity simulation results are to be released by the 1st of November.
Contacts
G. Barakos (Professor), George.Barakos@glasgow.ac.uk
G. Qiao (Research Assistant), g.qiao.1@research.gla.ac.uk
UoG Contributions to the GARTEUR AG 26 Group
Glasgow University is contributing to the AG26 team mainly via numerical simulations of the different experimental setups put forward.