IMPLEMENTATION OF WING ICE PROTECTION SYSTEM IN MORE ELECTRIC AIRCRAFT TECHNOLOGIES
MORE ELECTRIC AIRPLANE: CASE STUDY STOCKHOLM - COPENHAGEN
MORE ELECTRIC AIRCRAFT (MEA) SCALING ASPECTS AND WEIGHT IMPACT
Micro direct methanol fuel cell with perforated silicon-plate integrated ionomer membrane
Statistical Vortex-Generator-Jet Model for Turbulent Flow Separation Control
A Novel Modeling Approach for Vortex Generator Jet Flow Separation Control
Development and Validation of a Pt-Pd Diesel Oxidation Catalyst Model
2012-01-1286 Development and Validation of a Pt-Pd Diesel Oxidation Catalyst Model
2012-01-1294 Modeling of Dual Layer Ammonia Slip Catalysts (ASC)
Evaluation and Parameterization of Round Vortex Generator Jet Experiments for Flow Control
2011-01-1299 Development and Validation of a Cu-Zeolite SCR Catalyst Model
2011-01-1304 Fe-Zeolite SCR Model Development, Validation and Application
Evaluation of a Vortex Generator Model in Adverse Pressure Gradient Boundary Layers
2008-01-0613 Investigation on Uniformity Indices Used for Diesel Exhaust Aftertreatment Systems