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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.

    Date

    2024-10-17

    Time

    10:15

    Room

    Blue Hall 1

    IPC members
    • Co-Chair: Prof.Dr. Heji Huang, Institute of Mechanics, Chinese Academy of Sciences, China;

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

    • Rapporteur: Mr. Didier Boury, ArianeGroup SAS, France;

    • Rapporteur: Prof. Riheng Zheng, Beihang University, China;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    10:15

    Development status of the Air Turbo Rocket engine "ATRIUM”

    12

    confirmed

    Prof. Hiroaki Kobayashi

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    2

    10:27

    ADVANCES IN MIXING AND COMBUSTION MODELLING IN SUPERSONIC FLOWS

    12

    confirmed

    Mr. Sasi Kiran Palateerdham

    University of Rome “La Sapienza”

    Italy

    3

    10:39

    Multi-Objective Design Optimization of Fuel Injection Using Flexible Geometry for Scramjet-Powered Ascent Flight via Surrogate-Assisted Evolutionary Algorithms

    12

    confirmed

    Mr. Mehmet AKSAY

    Kyushu University

    Japan

    4

    10:51

    Experimental study on the combustion characteristics of multi-pintle injectors for annular combustor

    12

    confirmed

    Mr. Yaming Zhao

    School of Astronautics, Beihang University

    China

    5

    11:03

    physical insights into cavity flowfield in scramjet combustor via deep learning

    12

    confirmed

    Mr. Tomoaki NARA

    Kyushu University

    Japan

    6

    11:15

    Technological Challenges of the Design of a Scramjet Hypersonic Vehicle and its Flight Mission

    12

    confirmed

    Dr. Marco Marini

    CIRA Italian Aerospace Research Centre

    Italy

    7

    11:27

    Model-based knowledge discovery on design of Hypermixer fuel injectors for scramjet engines via deep-learning-based flowfield prediction

    12

    confirmed

    Mr. Chihiro Fujio

    Kyushu University

    Japan

    8

    11:39

    Integrated Flowpath Matching Design for Wide-Envelope Air-Breathing Launch Vehicles with RBCC Engines

    10

    confirmed

    Dr. jianlei wang

    Northwestern Polytechnical University

    China

    9

    11:49

    Study on low-cost prediction of the cavity flame holder flow field in a scramjet and its application to design optimization

    12

    confirmed

    Mr. Kotaro Iguchi

    Kanazawa Institute of Technology

    Japan

    10

    12:01

    flame stabilization in supersonic combustors

    12

    Prof. Akram Mohammad

    King Abdulaziz University

    Saudi Arabia

    11

    12:13

    Combined air-breathing and rocket propulsion system trajectory analysis for delivering payload to space

    12

    confirmed

    Dr. David Cerantola

    Space Engine Systems

    Canada

    12

    12:25

    Propulsive and combustion modelling of SABRE engine in air-breathing mode to support NOx emissions estimation in conceptual design

    12

    confirmed

    Mr. Fabrizio Borgna

    Politecnico di Torino

    Italy

    13*

    12:37

    Development of Turbo Jet Engine Heat Exchanger Code for TBCC Using Time-Dimensional Added Q1D Model

    12

    confirmed

    Dr. BOYEON KHIM

    Korea Aerospace Research Institute (KARI)

    Korea, Republic of

    14*

    12:37

    A SMALL LAUNCHER INCLUDING A DUAL MODE RAMJET AS SECOND STAGE

    12

    confirmed

    Mr. Lakshmi Narayana Phaneendra Peri

    Scuola di Ingegneria Aerospaziale "La Sapienza"

    Italy

    15*

    12:37

    EXPLORING THE PERFORMANCE OF INNOVATIVE SOLID FUEL RAMJETS

    12

    Mrs. Sai Gowthimi Kaluguru

    RMIT University (Royal Melbourne Institute of Technology)

    Australia