session 7

Title: Hypersonic Air-breathing and Combined Cycle Propulsion, and Hypersonic Vehicle
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, 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: Dr. Arnau Pons Lorente, Space Generation Advisory Council (SGAC), United States;
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1005	11:30	Optimised Inlet Design for Hypersonic Flights	15	withdrawn	Mr.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Injection Using Flexible Geometry for Scramjet-Powered Ascent Flight via Surrogate-Assisted Evolutionary Algorithms	15	withdrawn	Mr.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

session 7

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