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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

    3

    Evaluating heat release effects in a suprsonic reacting mixing layer with density fluctuation multiresolution analysis

    15

    no-show

    Dr. Wu Jiping

    College of Aerospace and Materials Engineering, National University of Defense Technology

    China

    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

    6

    An Unstructured RANS/Flamelet CFD solver for Numerical Simulation of the Supersonic Combustion in an Integrated ARI/GP Scramjet Combustor

    15

    no-show

    Dr. Bing Chen

    Beijing University of Aeronautics and Astronautics (BUAA)

    China

    7

    The study of fuel injector arrays for scramjet combustion

    15

    confirmed

    Dr. Haiyan WU

    China

    8

    DESIGN AND OPITMIZAITON OF HYDROCARBON-FUELED SCRAMJET STAR-UP SCHEME WITH EXPANSION CYCLE

    15

    no-show

    Mr. Hua Zhang

    College of Aerospace Science and Engineering, National University of Defense Technology

    China

    9

    Subassembly Matching Research and System Demonstration Tests of Air Turbo Rocket

    15

    no-show

    Mr. Ping LI

    Xi'an Aerospace Propulsion Institute

    China

    10

    Numerical simulation of a mach 6 airbreathing hypersonic flight test vehicle powered by triple-module scramjets

    15

    no-show

    Mr. Liang Jin

    China

    11

    The Role of Exergy Analysis in Scramjet Engine Performance Analysis and Optimation

    15

    no-show

    Mr. Siwei Dong

    College of Aerospace and Materials Engineering, National University of Defense Technology

    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

    DESIGN AND OPTIMIZATION OF HYDROCARBON-FUELED DUAL-MODE SCRAMJET WITH EXERGY ANALYSIS

    Mr. Wang Chao

    College of Aerospace and Materials Engineering, National University of Defense Technology

    China