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  • session 5

    Title

    Hypersonic and Combined Cycle Propulsion

    type

    oral

    Description

    This session includes papers dealing with use of air in earth-to-orbit propulsion.

    Date

    2011-10-06

    Time

    10:00

    Room

    TS-06

    IPC members
    • Chairman: Prof. Shigeru Aso, Kurume Institute of Technology, Japan;

    • Chairman: Mr. Norbert Puettmann, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany;

    • Rapporteur: Dr. Salvatore Borrelli, CIRA Italian Aerospace Research Centre, Italy;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Development Status of the Hypersonic Turbojet Engine for Mach 5 flight in JAXA

    15

    confirmed

    Dr. Hiroaki Kobayashi

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    2

    Cryogenic Fuel Management on the Precooled Turbo Jet Engine

    15

    confirmed

    Prof. Tetsuya Sato

    Waseda University

    Japan

    4

    Spark Ignition and Flame Propagation in a Low Pressure Ramjet Combustor with Cavity

    15

    confirmed

    Dr. Xi Wenxiong

    Science and Technology on Scramjet Laboratory, National University of Defense Technology

    China

    5

    Operational sensitivities of an integrated aerodynamic-ramp-injector/ gas-portfire flameholder in a supersonic combustor

    15

    confirmed

    Prof. xu xu

    Beihang University

    China

    5

    Operational sensitivities of an integrated aerodynamic-ramp-injector/ gas-portfire flameholder in a supersonic combustor

    15

    confirmed

    Dr. Baoxi Wei

    Beihang University

    China

    7

    The study of fuel injector arrays for scramjet combustion

    15

    confirmed

    Dr. Haiyan WU

    China

    12

    The multi-objective optimization design for two-dimensional variable scramjet engine cowl

    15

    confirmed

    Ms. Wang Qing

    College of Astronautics, Northwestern Polytechnical University

    China