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  1. Mixing Characteristics of Fuel Injection in Supersonic Combustor Considering Upstream Streamwise Vortices

    Article • March 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Jian Teng

  2. An Innovative Integration Concept for Forebody and Two-Dimensional Hypersonic Inlet with Controllable Wall Pressure Distribution

    Article • July 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Jian Teng

  3. Flow Distortion Generation and Management of an Axisymmetric Ramjet Engine

    Article • July 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Jian Teng