• Home
  • IAF Digital Library
  • Public Website
  • My papers
  • Home
  • event
  • IAC-17
  • C4
  • 9
  • session 9

    Title

    Hypersonic Air-breathing and Combined Cycle Propulsion

    type

    oral

    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

    14:45

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

    10

    confirmed

    Dr. Chengxiang Zhu

    Xiamen University

    China

    3

    15:05

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

    10

    confirmed

    Mr. Owen Pryor

    University of Central Florida (UCF)

    United States

    4

    15:15

    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

    6

    15:35

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

    10'

    confirmed

    Mr. Lazar T. Chitilappilly

    Vikram Sarabhai Space Centre (VSSC)

    7

    15:45

    An efficient approach for tomographic reconstruction in combustion diagnostics

    10

    confirmed

    Dr. Junling Song

    Equipment Academy

    China

    10

    16:15

    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

    16:25

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

    10

    confirmed

    Dr. Duo Zhang

    Northwestern Polytechnical University

    China

    13

    16:45

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

    10

    confirmed

    Dr. Fei XING

    Xiamen University

    China

    15

    17:05

    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

    17:15

    Performance of High Mach Number Scramjets - Tunnel vs Flight

    10

    confirmed

    Mr. Will Landsberg

    University of Queensland

    Australia

    17

    17:25

    Modeling Scramjet Supersonic Combustion via Eddy Dissipation Model

    10

    confirmed

    Mr. Jimmy-John Hoste

    University of Strathclyde

    United Kingdom