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    Numerical Investigation of Twin-Nozzle Rocket Plume Phenomenology, Part II

    Ebrahimi, H. / AIAA | British Library Conference Proceedings | 1998

    CFD Validation and Evaluation For Combustor and Nozzle Flow, Part II

    Ebrahimi, H. B. / AIAA | British Library Conference Proceedings | 1994

    High Fidelity Analysis of a Non-Reacting Pulsed Supersonic Combustor

    Malo-Molina, F. / Ebrahimi, H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    Numerical Parametric Analysis of a Generic Supersonic Combustor with a Modified Single Cavity

    Malo-Molina, F. / Ebrahimi, H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011

    A measurement archive for validation of the National Combustion Code

    Ebrahimi, H. / Ryder, Jr., R. / Brankovic, A. et al. | AIAA | 2001

    An Overview of Computational Fluid Dynamics for Application to Advanced Propulsion Systems

    Ebrahimi, H. B. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2004

    Numerical Investigation of Twin-Nozzle Rocket Plume Phenomenology

    Ebrahimi, H. B. / Levine, J. / Kawasaki, A. et al. | British Library Conference Proceedings | 1997

    Modeling of Pulse Detonation Engine Operation

    Mohanraj, R. / Merkle, C. L. / Ebrahimi, H. B. et al. | British Library Conference Proceedings | 2001

    NUMERICAL ANALYSIS OF A DIRECT CONNECT SUPERSONIC COMBUSTOR

    Malo-Molina, F. / Ebrahimi, H. / Gaitonde, D. et al. | British Library Conference Proceedings | 2011

    THREE DIMENSIONAL ANALYSIS OF A FULLY COUPLED HYPERSONIC AIR-BREATHING INLET-COMBUSTOR FLOWPATH

    Malo-Molina, F. / Gaitonde, D. / Ebrahimi, H. et al. | British Library Conference Proceedings | 2010

    Exploratory RANS and LES Simulations of Transient Supersonic Combustor Flow

    Ebrahimi, H. / Gaitonde, D. / Malo-Molina, F. et al. | British Library Conference Proceedings | 2009

    3-D Flowfield Structure in Generic Inward-Turning with Scramjet Combustor with Cavity

    Ebrahimi, H. / Gaitonde, D. / Malo-Molina, J. et al. | British Library Conference Proceedings | 2008

    Simulations of Hydrocarbon-Based Scramjet Combustors with Integrated Inward-Turning Inlets

    Ebrahimi, H. / Gaitonde, D. / Malo-Molina, F. et al. | British Library Conference Proceedings | 2008

    Parametric Study of 3-D Hydrocarbon Scramjet Engine with Cavity AIAA Paper

    Ebrahimi, H. / Gaitonde, D. / Malo-Molina, F. et al. | British Library Conference Proceedings | 2007

    Analysis of an Innovative Inward Turning Inlet Using an Air-JP8 Combustion Mixture at Mach 7

    Malo-Molina, F. / Ebrahimi, H. / Ruffin, S. et al. | British Library Conference Proceedings | 2006

    High Fidelity Flowpath Analysis of a Supersonic Combustor Coupled to Innovative Inward-Turning Inlets

    Malo-Molina, F. / Gaitonde, D. / Ebrahimi, H. et al. | British Library Conference Proceedings | 2009

    Simulation of 2-D and 3-D Multitube Pulse Detonation Engines with Conical Nozzle and Different Splitter Plates

    Ebrahimi, H. B. / Malo-Molina, F. J. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2005

    NUMERICAL INVESTIGATION OF 2-D AND 3-D MULTITUBE PULSE DETONATION USING H~2 AND JP8 FUEL

    Ebrahimi, H. B. / Malo-Molina, F. J. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2004