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  • session 9

    Title

    Hypersonic and Combined Cycle Propulsion

    Description

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

    Date

    2016-09-27

    Time

    14:45

    Room

    Zapopan

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

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

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    KEYNOTE: Shock Tunnel Development for Air-breathing Propulsion Testing at True Hypersonic Flight Conditions

    30'

    confirmed

    Mr. Zonglin Juang

    Institute of Mechanics, Chinese Academy of Sciences

    China

    2

    SABRE Technology Development

    15'

    confirmed

    Dr. Helen Webber

    Reaction Engines Ltd.

    United Kingdom

    3

    research on aerodynamic performance of a typical hypersonic inwardturning inlet

    15'

    confirmed

    Prof. Anyuan YU

    China Aerodynamics Research and Development Center (CARDC) 

    China

    4

    Preliminary Design and Performance Studies of a Wide Range Rocket-based Combined Cycle Engine

    15'

    confirmed

    Dr. Feiteng Luo

    Science and Technology on Scramjet Laboratory, Beijing Power Machinery Research Institute

    China

    5

    Development of an integrated platform for scramjet engine optimization design

    15'

    confirmed

    Mr. yuanguang wang

    Beijing Electro-Mechanical Engineering Institute, China Aerospace Science & Industry Corporation (CASIC)

    China

    6

    research on shock train leading edge detection in scramjet

    15'

    confirmed

    Mr. Chengyi Su

    Science and Technology on Scramjet Laboratory, Beijing Power Machinery Research Institute

    China

    7

    The Research of Air-Turbo-Rocket (ATR) Propulsion System Based on Double Solid Propellant Gas-Generator

    15'

    withdrawn

    Dr. yang LIU

    Science and Technology on Combustion, Internal Flow and Thermal-structure Laboratory, Northwestern Polytechnical University

    China

    8

    A Pre-cooled and Fuel-rich Pre-burned Mixed-flow Turbofan Cycle for Ground-to-Ma5 Engines

    15'

    withdrawn

    Dr. Wei Zhao

    Chinese Academy of Sciences

    China

    9

    Investigation of an Air Turborocket based Propulsion System

    15'

    confirmed

    Dr. Yen-Sen Chen

    American Institute of Aeronautics and Astronautics (AIAA)

    Taiwan, China

    10

    LIFE EVALUATION OF REUSABLE RAMJET ENGINE SUBJECTED TO CREEP-FATIGUE INTERACTION

    15'

    withdrawn

    Ms. Lili Fu

    School of Astronautics,Northwestern Polytechnical University

    China

    11

    mixing enhancement using secondary gas ejection method in supersonic-subsonic shear layer

    15'

    withdrawn

    Mr. Chenxi Zhang

    Northwestern Polytechnical University,NPU

    China

    12

    A Parallel Direct-Connect Test System for Solid Ducted Rocket

    15'

    confirmed

    Mr. Jiming Cheng

    Science and Technology on Combustion, Internal Flow and Thermal-structure Laboratory,Northwestern Polytechnical University

    China

    13

    Multi-Points Integrated Airframe/Engine Configuration Optimization of Hypersonic Vehicle

    15'

    withdrawn

    Ms. Qing Wang

    College of Mechanical and Electrical Engineering, Xi'an Polytechnic University

    China

    14

    airframe-propulsion integrated design and wind tunnel test for air-breathing hypersonic vehicle

    15'

    confirmed

    Mr. Zi-han Jiao

    China Academy of Launch Vehicle Technology (CALT)

    China

    15

    Performance evaluation and the status of TRRE

    15'

    confirmed

    Dr. Wenhui Ling

    Science and Technology on Scramjet Laboratory, Beijing Power Machinery Research Institute

    China

    16

    Design of Liquid Propellant Supply System with Wide Regulation Range of Primary Rocket in Rocket-Based Combined Cycle (RBCC) engine

    15'

    withdrawn

    Ms. Jingjing Bai

    China