IAF Digital Library

5

session 5

Title: Hypersonic and Combined Cycle Propulsion
type: oral
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	Mode	Presentation status	Speaker	Affiliation	Country
1		Aero-spike and RBCC Engine Systems for Future Space Transportation Vehicle	15'	confirmed	Mr. Tetsuo Hiraiwa	Japan Aerospace Exploration Agency (JAXA)	Japan
2		3D LES OF THE HYSHOT COMBUSTOR USING OPENFOAM	15'	withdrawn	Dr. Antonella Ingenito	University of Rome “La Sapienza”	Italy
3		SCRAMJET	15'	withdrawn	Mr. Alok Dand		India
4		Ramjet thruster using ozone dissociation energy for high altitude operation	15'	confirmed	Mr. Florin Mingireanu	Romanian Space Agency (ROSA)	Romania
5		Experiments of supersonic combustion using distributed injection in a model scramjet engine	15'	no-show	Dr. Sun Mingbo		China
6		Supersonic Combustion of Emerging Fuels	15'	no-show	Mr. Kalind Carpenter	California State University	United States
7		An experimental study on highly efficient ddt enhancement device for pde	15'	confirmed	Mr. Ryuji NAKAWATASE	Kyushu University	Japan
8		Numerical analysis of wave drag reduction by energy deposition in hypersonic flow	15'	withdrawn	Dr. Yu Xiao-Jing	Northwestern Polytechnical University	China
9		Effect of Pre-combustion Shock Train on Fuel Injection and Distribution in Scramjet	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	15'	confirmed	Ms. Jie Huang	China Aerodynamics Research and Development Center (CARDC)	China
10		Numerical and experiment study of the dynamic work process of a new type two-stage supersonic air ejector	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of primary rocket-assisted combustion under ramjet-mode condition in rocket based combined cycle (rbcc) engine	Poster	withdrawn	Mr.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	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	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	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	Poster	withdrawn	Dr. Xiaokang Li	National University of Defense Technology	China
16		Quasi-two-dimensional evaluation and optimization design for hypersonic scramjet propulsive flowpath	Poster	confirmed	Mr. Xin Ren	Science and Technology on Scramjet Laboratory, The 31st Research Institute of CASIC	China