IAF Digital Library

5

session 5

Title: Hypersonic and Combined Cycle Propulsion
Description: This session includes papers dealing with use of air in earth-to-orbit propulsion.
Date: 2011-10-06
Time: 10:00
Room: TS-06

IPC members

Chairman: Prof. Shigeru Aso, Kurume Institute of Technology, Japan;
Chairman: Mr. Norbert Puettmann, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany;
Rapporteur: Dr. Salvatore Borrelli, CIRA Italian Aerospace Research Centre, Italy;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		Development Status of the Hypersonic Turbojet Engine for Mach 5 flight in JAXA	15	confirmed	Dr. Hiroaki Kobayashi	Japan Aerospace Exploration Agency (JAXA)	Japan
2		Cryogenic Fuel Management on the Precooled Turbo Jet Engine	15	confirmed	Prof. Tetsuya Sato	Waseda University	Japan
3		Evaluating heat release effects in a suprsonic reacting mixing layer with density fluctuation multiresolution analysis	15	no-show	Dr. Wu Jiping	College of Aerospace and Materials Engineering, National University of Defense Technology	China
4		Spark Ignition and Flame Propagation in a Low Pressure Ramjet Combustor with Cavity	15	confirmed	Dr. Xi Wenxiong	Science and Technology on Scramjet Laboratory, National University of Defense Technology	China
5		Operational sensitivities of an integrated aerodynamic-ramp-injector/ gas-portfire flameholder in a supersonic combustor	15	confirmed	Dr. Baoxi Wei	Beihang University	China
6		An Unstructured RANS/Flamelet CFD solver for Numerical Simulation of the Supersonic Combustion in an Integrated ARI/GP Scramjet Combustor	15	no-show	Dr. Bing Chen	Beijing University of Aeronautics and Astronautics (BUAA)	China
7		The study of fuel injector arrays for scramjet combustion	15	confirmed	Dr. Haiyan WU		China
8		DESIGN AND OPITMIZAITON OF HYDROCARBON-FUELED SCRAMJET STAR-UP SCHEME WITH EXPANSION CYCLE	15	no-show	Mr. Hua Zhang	College of Aerospace Science and Engineering, National University of Defense Technology	China
9		Subassembly Matching Research and System Demonstration Tests of Air Turbo Rocket	15	no-show	Mr. Ping LI	Xi'an Aerospace Propulsion Institute	China
10		Numerical simulation of a mach 6 airbreathing hypersonic flight test vehicle powered by triple-module scramjets	15	no-show	Mr. Liang Jin		China
11		The Role of Exergy Analysis in Scramjet Engine Performance Analysis and Optimation	15	no-show	Mr. Siwei Dong	College of Aerospace and Materials Engineering, National University of Defense Technology	China
12		The multi-objective optimization design for two-dimensional variable scramjet engine cowl	15	confirmed	Ms. Wang Qing	College of Astronautics, Northwestern Polytechnical University	China
–		DESIGN AND OPTIMIZATION OF HYDROCARBON-FUELED DUAL-MODE SCRAMJET WITH EXERGY ANALYSIS			Mr. Wang Chao	College of Aerospace and Materials Engineering, National University of Defense Technology	China