Raffaele Donelli
Raffaele Donelli
Current Organizations / Institutes
The organizations/institutes from the scholar's latest article
Previous Organizations / Institutes
The organizations / institutes from the scholar's other articles in the past ten years
Research Subjects
Research Interests
Raffaele Donelli has a total of 68 co-authors. Here are the top co-authors by number of shared publications:
S. Hein
DLR, German Aerospace Center
5 shared publications- Ardeshir Hanifi
KTH Royal Institute of Technology
3 shared publications D. Arnal
ONERA, 31055 Toulouse, France
3 shared publications- Domenico Quagliarella
Italian Aerospace Research Centre
3 shared publications F. De Gregorio
3 shared publicationsJ. Quest
European Transonic Windtunnel
3 shared publications
Latest Publications
- 1 June 2013
- Published by Portico in International Journal of Flow Control
- Vol. 5 (2) , 89-110
Control of Flow with Trapped Vortices: Theory and Experiments
- 1 June 2013
- Published by Portico in International Journal of Flow Control
- Vol. 5 (2) , 89-110
Control of Flow with Trapped Vortices: Theory and Experiments
- 10 July 2011
- Published by Springer Nature in Experiments in Fluids
- Vol. 51 (5) , 1369-1384
Effects of a trapped vortex cell on a thick wing airfoil
- 10 July 2011
- Published by Springer Nature in Experiments in Fluids
- Vol. 51 (5) , 1369-1384
Effects of a trapped vortex cell on a thick wing airfoil
- 1 July 2011
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 48 (4) , 1147-1162
Design of a Supersonic Natural Laminar Flow Wing-Body
- 1 July 2011
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 48 (4) , 1147-1162
Design of a Supersonic Natural Laminar Flow Wing-Body
- 1 May 2010
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 47 (3) , 783-795
Design and Test of the UW-5006 Transonic Natural-Laminar-Flow Wing
- 1 May 2010
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 47 (3) , 783-795
Design and Test of the UW-5006 Transonic Natural-Laminar-Flow Wing
- 4 January 2010
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Flow Separation Control By Trapped Vortex
- 4 January 2010
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Flow Separation Control By Trapped Vortex