Stephane Bernard

发表

Control system for turbo machine of engine of aircraft, has switching unit comprising commutation modules and switches and switching between selected path and passive path in response to detection of failure by monitoring units

Stephane Bernard, Michael Dinsart, Xavier Flandrois, 2010 .

Statistical method for the determination of the ignition energy of dust cloud-experimental validation

Stephane Bernard, Kazimierz Lebecki, Philippe Gillard, 2010 .

Measurements for fuel reforming for scramjet thermal management and combustion optimization : status of the COMPARER project.

Marc Bouchez, Stephane Bernard, Emeric Daniau, 2006 .

Braking Systems with New IMA Generation

Jean-Pierre Garcia, Stephane Bernard, 2011 .

MIE and flame velocity of partially oxidised aluminium dust

Stephane Bernard, Fabrice Foucher, Philippe Gillard, 2012 .

Numerical and experimental validation of transient modelling for Scramjet active cooling with supercritical endothermic fuel

Marc Bouchez, Stephane Bernard, Emeric Daniau, 2006 .

Influence of the oxide content on the ignition energies of aluminium powders

Stephane Bernard, Philippe Gillard, P. Gillard, 2007 .

Characterisation of coking activity during supercritical hydrocarbon pyrolysis

Marc Bouchez, Stephane Bernard, Philippe Gillard, 2008 .

SFGP 2007 - Pyrolysis of Supercritical Endothermic Fuel: Evaluation for Active Cooling Instrumentation

Marc Bouchez, Stephane Bernard, Emeric Daniau, 2008 .