2/7/13    08:30 - 11:50 FP.09: Heat Transfer

TuM11 Room: Holiday Inn - Forum 15 Chair: Andrei Sidorenko Rapporteur: to be confirmed

Simulation of an Ablative Thermal Protection System for the Hypersonic Ascend of an Electromagnetically Launched Payload Carrier (*) D. Lancelle and O. Bozic Off-Stagnation Point Testing in Plasma Facility A. Viladegut and O. Chazot Evolution of turbulent heat flux across a shock wave R. Quadros, P. Sashittal, A. Ramachandran and K. Sinha Structure of a laminar viscous hypersonic gas flow over the delta wing with blunt leading edges. S. Alexandrov, A. Shalaev and A.V. Vaganov Influence of small spatial perturbations on heat transfer at hypersonic flow N. Palchekovskaya and V. Shvedchenko