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    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

    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

    A Navier-Stokes study of rotating stall in compressor cascades

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

    Reciprocal interactions of hairpin-shaped vortices and a boundary layer

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

    Navier-Stokes study of rotating stall in compressor cascades

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

    Reciprocal interactions of hairpin-shaped vortices and a boundary layer

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

    Direct Calculations of Waves in Fluid Flows Using High-Order Compact Difference Scheme

    Yu, S.-T. | Online Contents | 1994
    Beteiligte: Liu, N.-S.

    Benchmark test cases for the National Combustion Code

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

    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

    National Combustion Code - Parallel implementation and performance

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

    A study of hydrogen/air combustor using NCC

    Shih, T.-H. / NOrris, A. / Iannetti, A. et al. | AIAA | 2001

    Supersonic Flow Measurement and Computation of a Lobed-Mixer for Trapped Vortex Combusters

    Hendricks, R. / Liu, N.-S. / Shouse, D. et al. | British Library Conference Proceedings | 2001

    Supersonic flow measurement and computation of a lobed-mixer for trapped vortex combustors

    Brankovic, A. / Ryder, R.C. / Hendricks, R.C. et al. | IEEE | 2001

    Experimental and Computational Study of Trapped Vortex Combustor Sector Rig with High-Speed Diffuser Flow

    Hendricks, R.C. | Online Contents | 2001
    Beteiligte: Liu, N.-S.

    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

    EMISSIONS PREDICTION AND MEASUREMENT FOR LIQUID FUELED TVC COMBUSTOR WITH AND WITHOUT WATER INJECTION

    Brankovic, A. / Ryder, R. C. / Hendricks, R. C. et al. | British Library Conference Proceedings | 2005

    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

    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

    SPECIAL SECTION: COMBUSTION MODELING AND LARGE EDDY SIMULATION: DEVELOPMENT AND VALIDATION NEEDS FOR GAS TURBINES - Introduction: Combustion Modeling and Large Eddy Simulation: Development and Validation Needs for Gas Turbines

    Grinstein, F.F. | Online Contents | 2006
    Beteiligte: Liu, N.-S.

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