session 9

Title: Hypersonic and Combined Cycle Propulsion
Description: This session covers papers on Hypersonic and Combined Cycle Propulsion for space applications.
Date: 2014-09-30
Time: 14:45
Room: 714B

IPC members

Co-Chair: Mr. Patrick Danous, ArianeGroup, France;
Co-Chair: Prof. Riheng Zheng, Beihang University, China;
Rapporteur: Dr. Helen Webber, Reaction Engines Ltd., United Kingdom;

papers
Order	Time	Paper title	Selection result	Mode	Presentation status	Speaker	Affiliation	Country
1		progress of rocket based combined cycle in northwestern polytechnical university	accepted	15'	withdrawn	Prof. Guoqiang He	Northwestern Polytechnical University	China
2		Status of JAXA Combined-Cycle Engine Research for Future Space Transportation Vehicle	accepted	15'	confirmed	Mr. Shuichi Ueda	Japan Aerospace Exploration Agency (JAXA)	Japan
3		Numerical Analysis of Mode Transient Phenomena in a Rocked-Based Combined Cycle Engine	accepted	15'	withdrawn	Dr. Masatoshi Kodera	Japan Aerospace Exploration Agency (JAXA)	Japan
4		Experimental Study of the Unstart/Restart Process of Hypersonic Inlet Induced by Backpressure	accepted	15'	withdrawn	Dr. Yilong Zhao	Science and Technology on Scramjet Laboratory, National University of Defense Technology	China
5		large eddy simulation of the influence of primary rocket jet on low frequency combustion instability in a rocket-based combined-cycle engine	accepted	15'	withdrawn	Mr. Zhiwei Huang	Northwestern Polytechnical University,NPU	China
6		freejet test of a rocket based combined cycle engine at mach 3	accepted	15'	withdrawn	Mr. Lei Shi	College of Astronautics, Northwestern Polytechnical University	China
7		Design of a combined cycle airbreathing hypersonic engine for a simulated point-to-point mission: from concept selection to detailed design and optimisation.	accepted	15'	confirmed	Mr. Abhijeet Kumar	The University of Sydney	Australia
8		Supersonic combustion of liquid kerosene with an integrated strut-injector/cavity flameholder	accepted	15'	withdrawn	Mr. Wang Jianchen	Beihang University	China
9		Numerical Study of Vitiation Effects on Supersonic Combustion	accepted	15'	withdrawn	Mr. zhang yan	Beihang University	China
10		Ignition and flameholding characteristics of liquid alkane fuels in the supersonic combustor	accepted	15'	withdrawn	Mr. Liu Wei	Beihang University	China
11		study on the thermodynamic cycle characteristics of the Scramjet fuel feed system	accepted	15'	confirmed	Prof. Shen Chibing	National University of Defense Technology	China
12		Effects of Cowl and Cavity on Scramjet Fuel Mixing and Combustion	accepted	15'	withdrawn	Mr. Won Keun Chang	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
13		Flamelet modeling of two-phase n-decane supersonic combustion using a skeletal chemical reaction mechanism	accepted	15'	withdrawn	Mr. zhang yan	Beihang University	China