All Stories

  1. Ablation Model Based on Porous Charring Layer Under Alumina Erosion Condition

    Article • AIAA Journal, November 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Yang LIU, Zongyan Li

  2. Combustion Characteristics Experimental Study of Solid Hydrocarbon Propellant for Air-Turbo Rocket

    Article • Journal of Propulsion and Power, September 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Yang LIU

  3. A volumetric ablation model of EPDM considering complex physicochemical process in porous structure of char layer

    Article • Open Physics, June 2017, De Gruyter

    Dr. Yang LIU

  4. Study on the Thermal Decomposition Characteristics of AP/HTPB Composite Propellant under High Heat Flux

    Article • July 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Yang LIU

  5. “Thermal-Mechanical” Coupled Model Based on Porous Media Characteristics of EPDM insulator Char Layer

    Article • July 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Yang LIU

  6. Thermal analysis of RBCC engine at ejector, ramjet and scramjet modes

    Article • July 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Yang LIU

  7. An overall ablation model of ethylene-propylene-diene monomer based on porous characteristics in char layer

    Article • Advances in Mechanical Engineering, February 2016, SAGE Publications

    Dr. Yang LIU