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  • session 9

    Title

    Hypersonic and Combined Cycle Propulsion

    type

    oral

    Description

    This session covers papers on Hypersonic and Combined Cycle Propulsion for space applications.

    Date

    2014-09-30

    Time

    14:45

    Room

    714B

    IPC members
    • Co-Chair: Mr. Patrick Danous, ArianeGroup, France;

    • Co-Chair: Prof. Riheng Zheng, Beihang University, China;

    • Rapporteur: Dr. Helen Webber, Reaction Engines Ltd., United Kingdom;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    progress of rocket based combined cycle in northwestern polytechnical university

    15'

    withdrawn

    Prof. Guoqiang He

    Northwestern Polytechnical University

    China

    2

    Status of JAXA Combined-Cycle Engine Research for Future Space Transportation Vehicle

    15'

    confirmed

    Mr. Shuichi Ueda

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    3

    Numerical Analysis of Mode Transient Phenomena in a Rocked-Based Combined Cycle Engine

    15'

    withdrawn

    Dr. Masatoshi Kodera

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    4

    Experimental Study of the Unstart/Restart Process of Hypersonic Inlet Induced by Backpressure

    15'

    withdrawn

    Dr. Yilong Zhao

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

    China

    5

    large eddy simulation of the influence of primary rocket jet on low frequency combustion instability in a rocket-based combined-cycle engine

    15'

    withdrawn

    Mr. Zhiwei Huang

    Northwestern Polytechnical University,NPU

    China

    6

    freejet test of a rocket based combined cycle engine at mach 3

    15'

    withdrawn

    Mr. Lei Shi

    College of Astronautics, Northwestern Polytechnical University

    China

    7

    Design of a combined cycle airbreathing hypersonic engine for a simulated point-to-point mission: from concept selection to detailed design and optimisation.

    15'

    confirmed

    Mr. Abhijeet Kumar

    The University of Sydney

    Australia

    8

    Supersonic combustion of liquid kerosene with an integrated strut-injector/cavity flameholder

    15'

    withdrawn

    Mr. Wang Jianchen

    Beihang University

    China

    9

    Numerical Study of Vitiation Effects on Supersonic Combustion

    15'

    withdrawn

    Mr. zhang yan

    Beihang University

    China

    10

    Ignition and flameholding characteristics of liquid alkane fuels in the supersonic combustor

    15'

    withdrawn

    Mr. Liu Wei

    Beihang University

    China

    11

    study on the thermodynamic cycle characteristics of the Scramjet fuel feed system

    15'

    confirmed

    Prof. Shen Chibing

    National University of Defense Technology

    China

    12

    Effects of Cowl and Cavity on Scramjet Fuel Mixing and Combustion

    15'

    withdrawn

    Mr. Won Keun Chang

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    13

    Flamelet modeling of two-phase n-decane supersonic combustion using a skeletal chemical reaction mechanism

    15'

    withdrawn

    Mr. zhang yan

    Beihang University

    China