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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

    2021-10-28

    Time

    09:45

    Room

    Ajman D

    IPC members
    • Co-Chair: Mr. Arnau Pons Lorente, Space Generation Advisory Council (SGAC), Spain;

    • 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

    2

    09:45

    Control of shock wave boundary layer interaction by introducing wavy patches to the wall.

    15

    confirmed

    Mr. Debdoot Ghosh

    Vellore Institute of Technology

    India

    7

    10:00

    Numerical investigations of Fuel injection techniques in a cavity-based scramjet

    15

    confirmed

    Mr. Khaja Faisal Hussain

    Khalifa University of Science and Technology (KUST)

    United Arab Emirates

    10

    10:15

    Implementation of the ramjet control algorithm in the connected pipe test bench

    15

    confirmed

    Mr. Maurício Gontijo

    University of Brasilia

    Brazil

    11

    10:30

    Simulation of different mixture feeding regimes in a continuous wave detonation engine

    15

    confirmed

    Ms. Elena Mikhalchenko

    Scientific Research Institute for System Analysis, Russian Academy of Sciences (RAS)

    Russian Federation

    1001

    10:45

    Aerodynamic Characterization and Aerodatabase Development of STRATOFLY MR3 Hypersonic Vehicle

    15

    confirmed

    Dr. Pietro Roncioni

    CIRA Italian Aerospace Research Centre

    Italy

    1003

    11:00

    Space air breathing rocket engine

    15

    confirmed

    Mr. Prakhar Jain

    India

    1004

    11:15

    One Dimensional Model Simulation of Sramjet Engine Based on Multi-core Parallel Computation

    15

    confirmed

    Ms. Liu Yang

    CASIC

    China

    1005

    11:30

    Optimised Inlet Design for Hypersonic Flights

    15

    withdrawn

    Mr. Hitesh Dhawan

    University of Petroleum and Energy Studies

    India

    1006

    11:45

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

    15

    withdrawn

    Mr. Mehmet AKSAY

    Kyushu University

    Japan

    1008

    12:00

    Development of a Hypersonic Accelerator Vehicle (HAV) using Hybrid Propulsion System

    15

    withdrawn

    Prof. Élcio Jeronimo de Oliveira

    Luleå University of Technology

    Sweden

    1009

    12:15

    Design of regeneratively cooled combustion chamber a RBCC engine

    15

    withdrawn

    Dr. Tingting Jing

    Northwestern Polytechnical University,NPU

    China

    1012

    12:30

    Novel Pulse Detonation Engine Design for Optimized Performance and Energy Regeneration.

    15

    withdrawn

    Mr. Harmit Janak Vyas

    University of Petroleum and Energy Studies

    India

    *

    Design optimization and analysis of HTHL suborbital spaceplanes propelled by hybrid rocket motors

    withdrawn

    Mr. Mingyang Xiao

    Beihang University (BUAA)

    China

    *

    investigation on the regularities of VFDR working envelopes

    withdrawn

    Mr. Dong-xing HUO

    Academy of Aerospace Solid Propulsion Technology, China Aerospace Science and Technology Corporation (CASC)

    China