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    Assessment and Improvement of Engineering Simulation for Multiphase Turbulent Combustion in a Lean Direct Injection Combustor

    Liu, N.-S. | British Library Conference Proceedings | 2011

    SPECIAL SECTION: COMBUSTION MODELING AND LARGE EDDY SIMULATION: DEVELOPMENT AND VALIDATION NEEDS FOR GAS TURBINES - Turbulence Modeling for Very Large-Eddy Simulation

    Liu, N.-S. | Online Contents | 2006

    Numerical solution for the flow field of a body with jet

    LIU, N.-S. | AIAA | 1979

    Numerical solution of the Navier-Stokes equations for compressible turbulent two/three dimensional flows in the terminal shock region of an inlet/diffuser

    LIU, N.-S. / SHAMROTH, S. / MCDONALD, H. | AIAA | 1983

    Simulation of a Single-Element Lean-Direct Injection Combustor Using a Polyhedral Mesh Derived from Hanging-Node Elements

    Wey, C. / Liu, N.-S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2013

    SIMULATION OF AN INTEGRATED LEAN-DIRECT INJECTION COMBUSTOR AND A STAGE OF STATOR-ROTOR TURBINE

    Wey, C. / Liu, N.-S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011

    National Combustion Code - Parallel implementation and performance

    Quealy, A. / Ryder, R. / Norris, A. et al. | AIAA | 2000

    Dynamic response of shock waves in transonic diffuser and supersonicinlet - An analysis with the Navier-Stokes equations and adaptive grid

    LIU, N.-S. / SHAMROTH, S. / MCDONALD, H. | AIAA | 1984

    Reciprocal interactions of hairpin-shaped vortices and a boundary layer

    LIU, N.-S. / SHAMROTH, S. / MCDONALD, H. | AIAA | 1990

    The Effect of Spray Initial Conditions on Heat Release and Emissions in LDI CFD Calculations

    Iannetti, A. / Liu, N.-S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2008

    Benchmark test cases for the National Combustion Code

    Chen, K.-H. / Norris, A. / Quealy, A. et al. | AIAA | 1998

    Reciprocal interactions of hairpin-shaped vortices and a boundary layer

    LIU, N.-S. / SHAMROTH, S. J. / MCDONALD, H. | AIAA | 1991

    Time-Filtered Navier-Stokes Approach and Emulation of Turbulence-Chemistry Interaction

    Liu, N.-S. / Wey, T. / Shih, T.-H. et al. | British Library Conference Proceedings | 2013

    FILM COOLING FLOW EFFECTS ON POST-COMBOUSTOR TRACE CHEMISTRY

    Wey, T. / Liu, N.-S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2003

    A Navier-Stokes study of rotating stall in compressor cascades

    DAVOUDZADEH, F. / LIU, N.-S. / SHAMROTH, S. et al. | AIAA | 1988

    NASA Glenn Combustion Research for Aeronautical Propulsion

    Chang, C. T. / Tacina, K. / Lee, C. et al. | ASCE | 2013

    Navier-Stokes study of rotating stall in compressor cascades

    DAVOUDZADEH, F. / LIU, N.-S. / SHAMROTH, S. J. et al. | AIAA | 1990

    AIAA-2007-1268 COMPREHENSIVE COMBUSTION MODELING AND SIMULATION: RECENT PROGRESS AT NASA GLENN RESEARCH CENTER

    Liu, N.-S. / Shih, T.-H. / Wey, T. et al. | British Library Conference Proceedings | 2007

    The development of a variable Schmidt number model for jet-in-crossflows using genetic algorithms

    Guo, Yanhu / He, Guangbin / Hsu, Andrew et al. | AIAA | 1999

    A Strategy for Very Large Eddy Simulation of Complex Turbulent Flows (AIAA 2006-2099-2114)

    Shih, T.-H. / Liu, N.-S. / Chen, C.-L. et al. | British Library Conference Proceedings | 2006

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