1–19 of 19 hits
|

    RECONCILE DISCREPANCIES OF CURRENT SYNGAS KINETICS MODELS BY CONSIDERING TURBULENCE EFFECTS ON IGNITION DELAY AT GAS-TURBINE RELEVANT OPERATING CONDITIONS

    Ihme, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011

    Modeling Heatshield Erosion Due to Dust Particle Impacts for a Martian Entry Vehicle

    Palmer, G. E. / Ching, E. / Ihme, M. et al. | NTRS | 2019

    LES Investigation of Flow Field Sensitivity in a Gas Turbine Model Combustor (AIAA 2014-0621)

    See, Y.C. / Ihme, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2014

    Large-Eddy Simulation of a Gas Turbine Model Combustor

    See, Y.C. / Ihme, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2013

    Large-Eddy Simulations of a Dual-Mode Scramjet Combustor: Operating Point ``A'' of University of Virginia's Scramjet Experiments (AIAA 2014-1161)

    Chan, W.L. / Ihme, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2014

    Liquid Jet Instability Under Gravity Effects

    Amini, G. / Ihme, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2013

    Numerical Investigation of Detonation Transmission Mechanism based on High-order Discontinuous Galerkin Scheme (AIAA 2014-1505)

    Lv, Y. / Ihme, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2014

    Development of Discontinuous Galerkin Method for Detonation and Supersonic Combustion

    Lv, Y. / Ihme, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2013

    Characterization of Mixing and Ignition Effects in Flow-Reactor Facilities Using a Particle Method

    Weiher, S. / Ihme, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    Linear Stability Analysis of a Non-premixed Buoyant Jet Flame

    See, Y.C. / Ihme, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    Large Eddy Simulation of Supercritical Mixing and Combustion for Rocket Applications (AIAA 2014-0138)

    Hickey, J.-P. / Ihme, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2014

    Large-Eddy Simulation of a Turbulent Lifted Flame in a Vitiated Co-Flow

    Ihme, M. / See, Y. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2009

    Detailed Simulations of Shock-Bifurcation and Ignition of an Argon-diluted Hydrogen/Oxygen Mixture in a Shock Tube

    Ihme, M. / Sun, Y. / Deiterding, R. et al. | British Library Conference Proceedings | 2013

    Acoustic Behavior of a Partially-Premixed Gas Turbine Model Combustor

    Allison, P. / Driscoll, J. / Ihme, M. et al. | British Library Conference Proceedings | 2012

    LES of a Non-Premixed Flame Using an Extended Flamelet/Progress Variable Model

    Ihme, M. / Pitsch, H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2005

    Large-Eddy Simulation of Turbulent Reacting Flows

    Pitsch, H. / Desjardins, O. / Balarac, G. et al. | British Library Conference Proceedings | 2008