session 5

Title: Hypersonic and Combined Cycle Propulsion
Description: This session includes papers dealing with use of air in earth-to-orbit propulsion.
Date: 2012-10-04
Time: 10:15
Room: TS14 (Sala Capri, Palacongressi)

IPC members

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

papers
Order	Time	Paper title	Selection result	Mode	Presentation status	Speaker	Affiliation	Country
1		Aero-spike and RBCC Engine Systems for Future Space Transportation Vehicle	accepted	15'	confirmed	Mr. Tetsuo Hiraiwa	Japan Aerospace Exploration Agency (JAXA)	Japan
2		3D LES OF THE HYSHOT COMBUSTOR USING OPENFOAM	accepted	15'	withdrawn	Dr. Antonella Ingenito	University of Rome “La Sapienza”	Italy
3		SCRAMJET	accepted	15'	withdrawn	Mr. Alok Dand		India
4		Ramjet thruster using ozone dissociation energy for high altitude operation	accepted	15'	confirmed	Mr. Florin Mingireanu	Romanian Space Agency (ROSA)	Romania
5		Experiments of supersonic combustion using distributed injection in a model scramjet engine	accepted	15'	no-show	Dr. Sun Mingbo		China
6		Supersonic Combustion of Emerging Fuels	accepted	15'	no-show	Mr. Kalind Carpenter	California State University	United States
7		An experimental study on highly efficient ddt enhancement device for pde	accepted	15'	confirmed	Mr. Ryuji NAKAWATASE	Kyushu University	Japan
8		Numerical analysis of wave drag reduction by energy deposition in hypersonic flow	accepted	15'	withdrawn	Dr. Yu Xiao-Jing	Northwestern Polytechnical University	China
9		Effect of Pre-combustion Shock Train on Fuel Injection and Distribution in Scramjet	accepted	15'	no-show	Dr. Xi Wenxiong	Science and Technology on Scramjet Laboratory, National University of Defense Technology	China
10		Numerical and experiment study of the dynamic work process of a new type two-stage supersonic air ejector	accepted	15'	confirmed	Mr. Zonghao Wang	China Aerodynamics Research and Development Center (CARDC)	China
11		Experimental and numerical investigation of primary rocket-assisted combustion under ramjet-mode condition in rocket based combined cycle (rbcc) engine	accepted	Poster	withdrawn	Mr. Chaoqi Xu	Northwestern Polytechnical University	China
12		Analysis of the first stage trajectory for a TSTO space transportation concept powered by RBCC engine	accepted	Poster	confirmed	Mr. RUI XUE	College of Astronautics, Northwestern Polytechnical University	China
13		Aerodynamic Characteristics Research on the Waverider-based Hypersonic Vehicle with the Grid Fin	accepted	Poster	confirmed	Mr. Qing-Yang Guo	National University of Defense Technology	China
14		Thrust measure and capability analysis of H2/air mixture continuous rotating detonation wave model engine	accepted	Poster		Mr. Wei Lin	College of Aerospace and Materials Engineering, National University of Defense Technology	China
15		Study on thermal nonequilibrium laser-supported absorption wave and laser-powered air-breathing pulse detonation thruster	accepted	Poster	withdrawn	Dr. Xiaokang Li	National University of Defense Technology	China
16		Quasi-two-dimensional evaluation and optimization design for hypersonic scramjet propulsive flowpath	accepted	Poster	confirmed	Mr. Xin Ren	Science and Technology on Scramjet Laboratory, The 31st Research Institute of CASIC	China