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  • session 7

    Title

    Hypersonic Air-breathing and Combined Cycle Propulsion, and Hypersonic Vehicle

    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, detonation 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, together with the associated vehicle.

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

    • Co-Chair: Dr. Yen-Sen Chen, American Institute of Aeronautics and Astronautics (AIAA), United States;

    • Rapporteur: Mr. Simon Feast, Reaction Engines Ltd., United Kingdom;

    • Rapporteur: Mr. Jean-Claude Traineau, Office National d’Etudes et de Recherches Aérospatiales (ONERA), France;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    [KEYNOTE] The Synergetic Air-Breathing Rocket Engine (SABRE) - Development Status Update

    26

    Mr. Simon Feast

    Reaction Engines Ltd.

    United Kingdom

    2

    Design, combustion simulation and numerical analysis of the Rotating Detonation Engine

    11

    confirmed

    Ms. Kanika Dawar

    R V College of Engineering, Bengaluru

    India

    3

    three-dimensional numerical simulation of rotating detonation engine

    11

    confirmed

    Ms. Elena Mikhalchenko

    Scientific Research Institute for System Analysis, Russian Academy of Sciences (RAS)

    Russian Federation

    4

    effects of the pre-detonator on the stability of rotating detonation waves in a hollow combustion chamber

    11

    Dr. Wei Lin

    Space Engineering University (Beijing)

    China

    5

    Numerical study of JAXA’s experimental vehicle for hypersonic flight

    11

    confirmed

    Dr. Susumu Hasegawa

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    6

    Navier-Stokes Computation of Heat Transfer and Aero-heating Modeling for Hypersonic Waverider Vehicles

    11

    confirmed

    Mr. Nitish Kamal

    India

    7

    single and multiple retro-jet experiments in a hypersonic flow

    11

    confirmed

    Dr. Sungmin Lee

    Korea Aerospace Research Institute (KARI)

    Korea, Republic of

    8

    Experimental Studies on the Efficacy of Cavity with Porous Upper Surface in Controlling the Shock/Boundary-Layer Interactions in a Hypersonic Intake

    11

    confirmed

    Mr. Tamal Jana

    Indian Institute of Technology Kharagpur

    India

    9

    Laser Ignition of the Kerosene Containing Nano-Sized Aluminum in a Wide-speed-range Ramjet Combustor

    11

    confirmed

    Dr. Shaohua ZHU

    Northwestern Polytechnical University

    China

    10

    Investigation on Supersonic Combustion with Mach 10 Freeflow in Shock Tunnel

    11

    confirmed

    Mr. Liyin Wu

    China Aerodynamics Research and Development Center (CARDC) 

    China

    11

    LES OF AXIS SYMMETRIC AFT WALL ANGLE CAVITY IN SCRAMJETS

    11

    confirmed

    Dr. Antonella Ingenito

    Sapienza University of Rome

    Italy

    12

    Study on the mixing combustion performance of the secondary fuel injection for the afterburning chamber of the RBCC engine

    11

    withdrawn

    Prof. Dai Jian

    Central South University

    China

    13

    Numerical analysis on RBCC inlets of different types in ejector mode

    11

    confirmed

    Dr. Lei Shi

    Northwestern Polytechnical University,NPU

    China

    14

    EXPERIMENTAL STUDY OF RBCC ENGINE FUELED BY HYDROCARBON GEL ADDING NANO-ALUMINUM

    11

    withdrawn

    Dr. Duo Zhang

    Northwestern Polytechnical University

    China

    15

    Investigation on heat release matching and performance of variable geometry RBCC engine in ramjet mode

    11

    confirmed

    Dr. Jinying YE

    Northwestern Polytechnical University

    China

    16

    Numerical simulation research for the effects of trailing edge structure on the supersonic mixing layer

    confirmed

    Prof. Shen Chibing

    National University of Defense Technology

    China

    17

    AERODYNAMIC STUDY OF LARGE-SPACE INTEGRATED MORPHING AIRCRAFTS

    confirmed

    Dr. Dun Li

    China Academy of Aerospace Aerodynamics (CAAA)

    China

    18

    Development of an integrated TDLAS-based tomographic sensor for combustion diagnosis

    Dr. Junling Song

    Academy of Eqiupment

    China