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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

    2017-09-26

    Time

    14:45

    Room

    Hall E3

    IPC members
    • Co-Chair: Prof. Riheng Zheng, Beihang University, 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

    analysis on the performance of a hypersonic inward turning inlet with three combined channels

    10

    confirmed

    Dr. Chengxiang Zhu

    Xiamen University

    China

    2

    Highly reliable life time evaluation approaches for ramjet booster stage of next reusable launch vehicle

    10

    no-show

    Mr. ren jiawan

    China

    3

    Development of optical diagnostics for the characterization of high-velocity combustion

    10

    confirmed

    Mr. Owen Pryor

    University of Central Florida (UCF)

    United States

    4

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

    10

    confirmed

    Dr. Wei Zhao

    Chinese Academy of Sciences

    China

    5

    Thermodynamic Analysis of Helium System Cycle for the Precooled Air-breathing Combined Engine

    10

    no-show

    Dr. Yuan Ma

    Xi'an Aerospace Propulsion Institute

    China

    6

    Successful Flight Testing of Scramjet Engine Over Wide Range of Test Conditions

    10'

    confirmed

    Mr. Lazar T. Chitilappilly

    Vikram Sarabhai Space Centre (VSSC)

    7

    An efficient approach for tomographic reconstruction in combustion diagnostics

    10

    confirmed

    Dr. Junling Song

    Equipment Academy

    China

    8

    Numerical Simulation in Operation Matching Characteristics of Inlet and Compressor for Air Turbo Rocket

    10

    withdrawn

    Dr. YANG LIU

    China

    9

    Researches on Rocket-Based Combined-Cycle Inlet in Northwestern Polytechnical University

    10

    withdrawn

    Dr. Lei Shi

    Northwestern Polytechnical University,NPU

    China

    10

    Performance Optimization Method of Turbocharged Solid Propellant Ramjet(TSPR)

    10

    confirmed

    Dr. Wei Wang

    1. Systems Engineering Institute of Sichuan Aerospace; 2.Science and Technology on Combustion, Internal Flow and Thermal-Structure Laboratory, Northwestern Polytechnical University

    China

    11

    a novel liquid rocket-ramjet combined-cycle engine enhanced by a compact internal air turborocket

    10

    confirmed

    Dr. Duo Zhang

    Northwestern Polytechnical University

    China

    12

    Numerical investigation on the full flowpath performance of RBCC engine

    10

    withdrawn

    Mr. Ya Jun Wang

    College of Astronautics, Northwestern Polytechnical University

    China

    13

    Tomography for two-dimensional gas temperature distribution based on tunable diode laser absorption spectroscopy

    10

    confirmed

    Dr. Fei XING

    Xiamen University

    China

    14

    Cycle analysis and optimization of the precooled Air Turbo-Ramjet

    10

    withdrawn

    Prof.Dr. Jiang Qin

    Harbin Institute of Technology

    China

    15

    Performance Analysis of RBCC-Based TSTO Space Transportation Systems via Multi-Objective Design Optimisation

    10

    confirmed

    Mr. Philipp Klink

    RMIT University (Royal Melbourne Institute of Technology)

    Australia

    16

    Performance of High Mach Number Scramjets - Tunnel vs Flight

    10

    confirmed

    Mr. Will Landsberg

    University of Queensland

    Australia

    17

    Modeling Scramjet Supersonic Combustion via Eddy Dissipation Model

    10

    confirmed

    Mr. Jimmy-John Hoste

    University of Strathclyde

    United Kingdom

    18

    TRRE Technology Development

    10

    withdrawn

    Dr. Wenhui Ling

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

    China

    19

    experimental research on behavior of a non-premixed rotating detonation engine

    10

    withdrawn

    Dr. Yu YAN

    Xi'an aerospace propulsion institure

    China