Application challenge	Contributors	Organization
Transition effect on a shock-wave/boundary layer interaction	Reynald Bur and Eric Garnier	EUROMECH
Transonic Turbulent flow in a 3D channel with a swept bump	Vincent Couaillier	EUCASS
Aero-thermal analysis of combustor/turbine interaction in aero-engines: the challenge of today	Massimiliano Insinna, Simone Salvadori, Francesco Martelli, Paolo Adami, and Raul Vazquez	EUROTURBO
Drag reduction for three dimensional wing at transonic speed	Ning Qin	CEAS
A common platform for validation of aircraft drag reduction technologies	Daniel Redondo	ECCOMAS