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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

    2019-10-25

    Time

    09:45

    Room

    143A

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

    • Co-Chair: Ms. Elizabeth Driscoll, GomSpace Aps, United States;

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

    • 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

    09:45

    KEYNOTE: Test Complex M11: Research on Future Orbital Propulsion Systems and Scramjet Engines

    24

    confirmed

    Mr. Marius Wilhelm

    German Aerospace Center (DLR)

    Germany

    2

    10:09

    Ultra-fast laser-absorption techniques for performance characterization of advanced airbreathing hypersonic propulsion systems

    11

    confirmed

    Prof. Subith Vasu

    University of Central Florida (UCF)

    United States

    3

    10:20

    Bantam After Burning Rocket Engine (ABRE) propulsion system for a reusable hypersonic test bed

    11

    withdrawn

    Mr. Joaquin Castro

    Aerojet Rocketdyne

    United States

    4

    10:31

    CFD Analysis of Supersonic Turbulent Compressible Flows with detailed Plume Structure for Single and Multi-Nozzles for Aerospace Vehicles Design

    11

    withdrawn

    Dr. Muhammad Amjad Sohail

    Other

    Pakistan

    5

    10:42

    Chemical time scales distribution for scramjet operation

    11

    confirmed

    Prof. Sterian Danaila

    University POLITEHNICA of Bucharest - Research Center for Aeronautics and Space

    Romania

    6

    10:53

    Development of rocket-ramjet propulsion based on continuously rotating detonation

    11

    confirmed

    Prof. Piotr Wolanski

    Polish Academy of Sciences

    Poland

    7

    11:04

    Dynamic Modeling of Ramjet Engine Based on Simulated Annealing Algorithm

    11

    withdrawn

    Ms. Qin Yan-ping

    Xi'an Aerospace Propulsion Institute

    China

    8

    11:15

    Experimental Investigation of Hydrocarbon Based Fuels in Solid Fuel Ramjet Propulsion

    11

    confirmed

    Dr. Olexiy Shynkarenko

    University of Brasilia

    Brazil

    9

    11:26

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

    11

    confirmed

    Prof. Shen Chibing

    National University of Defense Technology

    China

    10

    11:37

    Fuzzy Control of Shock Position of wide range ramjet

    11

    withdrawn

    Ms. Qin Yan-ping

    Xi'an Aerospace Propulsion Institute

    China

    11

    11:48

    Numerical investigation on Nonlienar Dynamic Response of the Ramjet Engine to freestream perturbations based on WENO scheme

    11

    withdrawn

    Ms. Qin Yan-ping

    Xi'an Aerospace Propulsion Institute

    China

    12

    11:59

    CFD Investigation of Ramjet Flameholder Near-wake Flow Based on OpenFOAM Framework

    11

    confirmed

    Mr. Sigang Yu

    Northwestern Polytechnical University

    China

    13

    12:10

    PROGRESS ON COMPUTATIONAL DISINTEGRATION AND SEPARATION PROCESS FOR HYPERSONIC VEHICLE

    11

    confirmed

    Dr. Dun Li

    China Academy of Aerospace Aerodynamics (CAAA)

    China

    14

    12:21

    Research on Boundary Layer Combustion for Skin-Friction Reduction

    11

    Mr. RUI XUE

    College of Astronautics, Northwestern Polytechnical University (NPU)

    China

    15

    12:32

    Numerical Simulation of Turbulent Flow and Combustion in Ramjet Chamber with Non-uniform Inflow

    11

    confirmed

    Mr. Sigang Yu

    Northwestern Polytechnical University

    China