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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

    2022-09-21

    Time

    10:15

    Room

    W08

    IPC members
    • Co-Chair: Dr. Toru Shimada, Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency, Japan;

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

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

    • Rapporteur: Mr. Martin Velander, GKN Aerospace Engine Systems, Sweden;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    10:15

    design of a highly reusable air turbo-rocket engine

    15

    confirmed

    Mr. Ferran Roig Tió

    Destinus

    Switzerland

    2

    10:30

    Preliminary Design Procedure of Gun Launched Solid Fuel Ramjet Propulsion System

    15

    confirmed

    Mr. Seungho Lee

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    3

    10:45

    CONCEPTUAL DESIGN PREDICTION OF PROPULSIVE PERFORMANCES AND POLLUTANT EMISSIONS FOR HYBRID AIR-BREATHING/ROCKET ENGINES: A STUDY ON SABRE

    15

    confirmed

    Mr. Giovanni Grimaldi

    Politecnico di Torino

    Italy

    4

    11:00

    Concept design of a combined cycle hydrolox engine for commercial suborbital spaceflight applications

    15

    confirmed

    Mr. Mattia Bertolini

    Politecnico di Milano

    Italy

    5

    11:15

    Multi-Objective Design Optimization of Fuel Injection with Flexible Geometry via Surrogate-Based Evolutionary Algorithms Using Highly Parallel GPU Architecture

    15

    confirmed

    Mr. Mehmet AKSAY

    Kyushu University

    Japan

    6

    11:30

    NUMERICAL ANALYSIS OF ROCKET STAGED COMBUSTION WITH AIR-STAGED AND FUEL-STAGED SUPPLIES FOR HIGH-COMBUSTION PERFORMANCE AND LOW-POLLUTANT EMISSIONS

    15

    confirmed

    Mr. ILYES GHEDJATTI

    Beijing University of Aeronautics and Astronautics (BUAA)

    China

    7

    11:45

    Research on the effect of asymmetric air intake on the mixing and combustion of solid ramjet

    15

    confirmed

    Mr. Pu Shi

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

    China

    8

    12:00

    LES INVESTIGATION OF A CAVITY-BASED AXSYMMERIC SCRAMJET

    15

    confirmed

    Mr. Naresh Relangi

    Scuola di Ingegneria Aerospaziale "La Sapienza"

    Italy

    9

    12:15

    Optimized Inlet Design for Hypersonic Flights

    15

    confirmed

    Mr. Paras Adlakha

    University of Petroleum and Energy Studies

    India

    10

    12:30

    Assessment of Shock/Boundary-Layer Interactions in Hypersonic Intake

    15

    Dr. Mrinal Kaushik

    Indian Institute of Technology Kharagpur

    India