session 9

Title: Hypersonic Air-breathing and Combined Cycle Propulsion
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, denotation 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.
Date: 2018-10-02
Time: 14:45
Room: ZARM 5

IPC members

Co-Chair: Prof. Riheng Zheng, Beihang University, China;
Co-Chair: Dr. Helen Webber, Reaction Engines Ltd., United Kingdom;
Rapporteur: Dr. Salvatore Borrelli, CIRA Italian Aerospace Research Centre, Italy;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	14:45	KEYNOTE: Advance of Scramjet Operating Mode Comprehension based on Shock Tunnel Experiments and Numerical Modelling	26	confirmed	Prof.Dr. Klaus Hannemann	DLR, German Aerospace Center	Germany
2	15:11	Numerical Study of the Improvement of the Ejector-jet Performance in the RBCC Engine Combustor Model	14	withdrawn	Dr. Susumu Hasegawa	Japan Aerospace Exploration Agency (JAXA)	Japan
3	15:25	an integrated turbopump feed system based on gas generator cycle for RBCC in multiple modes	14	confirmed	Prof.Dr. Hongliang Pan	Northwestern Polytechnical University	China
4	15:39	Flow and thermal characteristics in regenerative cooling channels around cavity of RBCC	14	confirmed	Dr. Tingting Jing	Northwestern Polytechnical University	China
5	15:53	Experimental study of RBCC engine fueled by hydrocarbon gel adding nano-aluminum	14	withdrawn	Dr. Duo Zhang	Northwestern Polytechnical University	China
6	16:07	Design and analysis of a four-ducts inward turning inlet for XTENDER engine	14	withdrawn	Dr. Chengxiang Zhu	Xiamen University	China
7	16:21	Heat transfer enhancement of supercritical hydrocarbon fuel in regenerative cooling channels with micro-ribs of scramjet	14	confirmed	Ms. xin li	Harbin Institute of Technology	China
8	16:35	Multi-fidelity analysis of hydrogen-fueled scramjets to predict emissions	14	withdrawn	Mr. Jimmy-John Hoste	University of Strathclyde	United Kingdom
9	16:49	Numerical simulation study on the scalar mixing characteristics in supersonic mixing layers	14	confirmed	Prof. Shen Chibing	National University of Defense Technology	China
10	17:03	Research on Dynamic Characteristics and Control Scheme of Kerosene-Based Scramjet System	14	confirmed	Mr. Xuan Jin	National University of Defense Technology	China
11	17:17	The resolution analysis of Tunable Diode Laser Absorption Spectroscopy system for velocity measurement of the scramjet combustion flow	14	confirmed	Dr. Wei Rao	Academy of Eqiupment	China
12	17:31	Numerical investigations on the improvement of burning conditions in the scramjet	14	confirmed	Prof. Sterian Danaila	University POLITEHNICA of Bucharest - Research Center for Aeronautics and Space	Romania
13	17:45	Lattice Boltzmann simulation of a kerosene droplet impact on wall of combustion chamber in RBCC	14	withdrawn	Dr. Yan Ba	Northwestern Polytechnical University	China
14	17:59	Numerical Investigation on the Mixing Characteristics of Shear Layers in Supersonic-Subsonic Flow	14	confirmed	Dr. Kai Ma	Northwestern Polytechnical University	China
15	18:13	Simulation of supersonic combustion based on Very-Large Eddy Simulation method	14	withdrawn	Prof. Xingsi Han	Nanjing University of Aeronautics and Astronautics	China

session 9

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