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  • session 9

    Title

    Hypersonic Air-breathing and Combined Cycle Propulsion

    Description

    This session covers hypersonic air-breathing and combined cycle propulsion with space applications. The typical types of engine considered in this session include: turbojet, ramjet, Scramjet, denotation engine, Turbine Based Combined Cycle (TBCC), Rocket Based Combined Cycle (RBCC), Hypersonic Pre-cooled Propulsion, Air Turbo Rocket (ATR) and other types of hypersonic combined cycle propulsion.

    Date

    2018-10-02

    Time

    14:45

    Room

    ZARM 5

    IPC members
    • Co-Chair: Dr. Riheng Zheng, China Aerospace Science & Industry Corporation (CASIC), China;

    • Co-Chair: Dr. Helen Webber, Reaction Engines Ltd., United Kingdom;

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    14:45

    KEYNOTE: Advance of Scramjet Operating Mode Comprehension based on Shock Tunnel Experiments and Numerical Modelling

    26

    confirmed

    Prof.Dr. Klaus Hannemann

    DLR, German Aerospace Center

    Germany

    2

    15:11

    Numerical Study of the Improvement of the Ejector-jet Performance in the RBCC Engine Combustor Model

    14

    withdrawn

    Dr. Susumu Hasegawa

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    3

    15:25

    an integrated turbopump feed system based on gas generator cycle for RBCC in multiple modes

    14

    confirmed

    Prof.Dr. Hongliang Pan

    Northwestern Polytechnical University

    China

    4

    15:39

    Flow and thermal characteristics in regenerative cooling channels around cavity of RBCC

    14

    confirmed

    Dr. Tingting Jing

    Northwestern Polytechnical University

    China

    5

    15:53

    Experimental study of RBCC engine fueled by hydrocarbon gel adding nano-aluminum

    14

    withdrawn

    Dr. Duo Zhang

    Northwestern Polytechnical University

    China

    6

    16:07

    Design and analysis of a four-ducts inward turning inlet for XTENDER engine

    14

    withdrawn

    Dr. Chengxiang Zhu

    Xiamen University

    China

    7

    16:21

    Heat transfer enhancement of supercritical hydrocarbon fuel in regenerative cooling channels with micro-ribs of scramjet

    14

    confirmed

    Ms. xin li

    Harbin Institute of Technology

    China

    8

    16:35

    Multi-fidelity analysis of hydrogen-fueled scramjets to predict emissions

    14

    withdrawn

    Mr. Jimmy-John Hoste

    University of Strathclyde

    United Kingdom

    9

    16:49

    Numerical simulation study on the scalar mixing characteristics in supersonic mixing layers

    14

    confirmed

    Prof. Shen Chibing

    National University of Defense Technology

    China

    10

    17:03

    Research on Dynamic Characteristics and Control Scheme of Kerosene-Based Scramjet System

    14

    confirmed

    Mr. Xuan Jin

    National University of Defense Technology

    China

    11

    17:17

    The resolution analysis of Tunable Diode Laser Absorption Spectroscopy system for velocity measurement of the scramjet combustion flow

    14

    confirmed

    Dr. Wei Rao

    Academy of Eqiupment

    China

    12

    17:31

    Numerical investigations on the improvement of burning conditions in the scramjet

    14

    confirmed

    Prof. Sterian Danaila

    University POLITEHNICA of Bucharest - Research Center for Aeronautics and Space

    Romania

    13

    17:45

    Lattice Boltzmann simulation of a kerosene droplet impact on wall of combustion chamber in RBCC

    14

    withdrawn

    Dr. Yan Ba

    Northwestern Polytechnical University

    China

    14

    17:59

    Numerical Investigation on the Mixing Characteristics of Shear Layers in Supersonic-Subsonic Flow

    14

    confirmed

    Dr. Kai Ma

    Northwestern Polytechnical University

    China

    15

    18:13

    Simulation of supersonic combustion based on Very-Large Eddy Simulation method

    14

    withdrawn

    Prof. Xingsi Han

    Nanjing University of Aeronautics and Astronautics

    China