session 9

Title: Hypersonic and Combined Cycle Propulsion
Description: This session covers papers on space propulsion application and R&D with a wide range of interest.
Date: 2013-09-24
Time: 14:45
Room: 208A

IPC members

Chairman: Dr. Salvatore Borrelli, CIRA Italian Aerospace Research Centre, Italy;
Chairman: Prof. Shigeru Aso, Kurume Institute of Technology, Japan;
Rapporteur: Mr. Patrick Danous, ArianeGroup, France;

papers
Order	Time	Paper title	Selection result	Mode	Presentation status	Speaker	Affiliation	Country
1		Combined Cycle Propulsion System?Challenge and Prospects	accepted	15'	confirmed	Mr. zhang chengzhi	China Academy of Launch Vehicle Technology (CALT)	China
2		Computational Investigation of effect of Converging-Diverging Nozzle (C-D Nozzle) on the Performance of Pulse Detonation Engine(PDE)- Effects on Thrust and Inlet Pressure	accepted	15'		Dr. Ugur Guven		United States
3		Comprehensive Consideration of Gelled fuel in hypersonic ramjet propulsion	accepted	15'	withdrawn	Dr. Jianxin HU		China
4		The constant pressure time in a piston driver of free piston shock tunnel	accepted	15'		Dr. Zhu Hao	China Academy of Aerospace Aerodynamics (CAAA)	China
5		experimental study on rbcc with oxygen/kerosene firstly combustion	accepted	15'	confirmed	Dr. Liang Tian	Beihang University	China
6		Measurements of two-dimensional temperature distribution in combustion using diode laser absorption spectroscopy	accepted	15'	confirmed	Dr. Junling Song	Academy of Equipment	China
7		Influencing Factors on the Mode Transition in a Dual-Mode Scramjet Combustor	accepted	15'	confirmed	Mr. zhang yan	Beihang University	China
8		Mixing and combustion characteristics with lobe nozzel upstream of a V-gutter in a subsonic flow	accepted	15'	withdrawn	Ms. yanan Wang	National University of Defense Technology	China
9		System Design and Analysis of Hydrocarbon Scramjet with Regeneration Cooling and Expansion Cycle	accepted	15'		Dr. Wu Xianyu	College of Aerospace and Materials Engineering, National University of Defense Technology	China
10		CALCULATION OF AERODYNAMIC CHARACTERISTICS OF SAME MODEL SWIVEL NOZZLES WITH MATHEMATICAL MODELING OF REAL GAS EFFECTS	accepted	15'	confirmed	Dr. Alexey Galaktionov	Central Research Institute for Machine Building (JSC TSNIIMASH)	Russian Federation
11		Thermodynamic limitation on boron energy realization in ramjet propulsion	accepted	15'	confirmed	Prof. Alon Gany	TECHNION - Israel Institute of Technology	Israel
12		Thermal decomposition of model endothermic hydrocarbon fuels and their mixtures	accepted	15'	confirmed	Dr. Rongpei Jiang	Beijing Institute of Aerospace Testing Technology	China
13		Experimental Investigation on Angled Transverse Liquid Jet in Supersonic Crossflow	accepted	15'	confirmed	Mr. Tong Yiheng	College of Aerospace and Materials Engineering, National University of Defense Technology	China