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.

IPC members

Co-Chair: Prof. Riheng Zheng, Beihang University, China;
Co-Chair: Dr. Yen-Sen Chen, American Institute of Aeronautics and Astronautics (AIAA), United States;
Rapporteur: Mr. Simon Feast, British Interplanetary Society, United Kingdom;
Rapporteur: Mr. Jean-Claude Traineau, Office National d’Etudes et de Recherches Aérospatiales (ONERA), France;

papers
Order	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	KEYNOTE: The Synergetic Air-Breathing Rocket Engine (SABRE) - Development Status Update	30	confirmed	Mr. Simon Feast	Reaction Engines Ltd.	United Kingdom
2	Design, combustion simulation and numerical analysis of the Rotating Detonation Engine	10	confirmed	Ms. Kanika Dawar	R V College of Engineering, Bengaluru	India
3	three-dimensional numerical simulation of rotating detonation engine	10	confirmed	Ms. Elena Mikhalchenko	Scientific Research Institute for System Analysis, Russian Academy of Sciences (RAS)	Russian Federation
5	Numerical study of JAXA’s experimental vehicle for hypersonic flight	10	confirmed	Dr. Susumu Hasegawa	Japan Aerospace Exploration Agency (JAXA)	Japan
6	Navier-Stokes Computation of Heat Transfer and Aero-heating Modeling for Hypersonic Waverider Vehicles	10	confirmed	Mr. Nitish Kamal		India
7	single and multiple retro-jet experiments in a hypersonic flow	10	confirmed	Dr. Sungmin Lee	Korea Aerospace Research Institute (KARI)	Korea, Republic of
8	Experimental Studies on the Efficacy of Cavity with Porous Upper Surface in Controlling the Shock/Boundary-Layer Interactions in a Hypersonic Intake	10'	confirmed	Mr. Tamal Jana	Indian Institute of Technology Kharagpur	India
9	Laser Ignition of the Kerosene Containing Nano-Sized Aluminum in a Wide-speed-range Ramjet Combustor	10	confirmed	Dr. Shaohua ZHU	Northwestern Polytechnical University	China
10	Investigation on Supersonic Combustion with Mach 10 Freeflow in Shock Tunnel	10	confirmed	Mr. Liyin Wu	China Aerodynamics Research and Development Center (CARDC)	China
11	LES OF AXIS SYMMETRIC AFT WALL ANGLE CAVITY IN SCRAMJETS	10	confirmed	Mr. Naresh Relangi	Scuola di Ingegneria Aerospaziale "La Sapienza"	Italy
13	Numerical analysis on RBCC inlets of different types in ejector mode	10	confirmed	Dr. Lei Shi	Northwestern Polytechnical University，NPU	China
15	Investigation on heat release matching and performance of variable geometry RBCC engine in ramjet mode	10	confirmed	Dr. Jinying YE	Northwestern Polytechnical University	China
16	Numerical simulation research for the effects of trailing edge structure on the supersonic mixing layer	10	confirmed	Prof. Shen Chibing	National University of Defense Technology	China
17	AERODYNAMIC STUDY OF LARGE-SPACE INTEGRATED MORPHING AIRCRAFTS	10	confirmed	Dr. Dun Li	China Academy of Aerospace Aerodynamics (CAAA)	China

session 7

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