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. It is a joint ISOABE/IAF session.
Date: 2008-10-02
Time: 10:00
Room: Dochart 2

IPC members

Chairman: Mr. William W. Smith, Aerojet Rocketdyne, United States;
Chairman: Prof. Nobuhiro Tanatsugu, Muroran Institute of Technology, Japan;
Rapporteur: Prof. Shigeru Aso, Kurume Institute of Technology, Japan;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		Heat Exchanger Design in Combined Cycle Engines Helen Webber and Simon Feast Reaction Engines Ltd., D5 Culham Science Centre, Abingdon, Oxon, OX14 3DB, UK	presentation		Dr. Helen Webber	Reaction Engines Ltd.	United Kingdom
2		Heat Exchanger Development at Reaction Engines Ltd.	discussion		Mr. Richard Varvill	Reaction Engines Ltd.	United Kingdom
3		Design and Testing of the Contra-rotating Turbine for the SCIMITAR Precooled Engine	presentation		Mr. Richard Varvill	Reaction Engines Ltd.	United Kingdom
4		Development Study of A Precooled Turbojet Engine	presentation		Prof. Tetsuya Sato	Waseda University	Japan
5		french r&t effort for high-speed airbreathing propulsion status in 2008	presentation		Mr. Francois FALEMPIN	MBDA France	France
6		fully axisymmetric airbreather concept for space launcher first application to a micro-space launcher	discussion		Mr. Francois FALEMPIN	MBDA France	France
7		Proposals justification to combined rocket engines application as a part of aerospace system	presentation		Dr. Olexiy Shynkarenko	Dniepropetrovsk National University	Brazil
8		Design and Optimization of Two-Stage-To-Orbit Launch Vehicle with Air Turbo Rocket Propulsion	presentation		Dr. Chunlin Gong	Northwestern Polytechnical University	China
9		supersonic combustion enhancement by shock wave impingement for scram-jet engine	presentation		Mr. Arif Nur Hakim	Indonesian National Institute of Aeronautics and Space (LAPAN)	Indonesia
10		Numerical investigation of the configuration effects to the Ejector-jet Performance in the RBCC engine combustor model	discussion		Dr. Susumu Hasegawa	Japan Aerospace Exploration Agency (JAXA)	Japan
11		Numerical Simulation of MHD Flows in 2-D Scramjet Inlets	discussion		Dr. Zheng Xiaomei		China
12		3-D Numerical Simulation for Ramjet using an efficient Multi-Code CFD Solver	discussion		Mr. Yue Chuan	Beijing University of Aeronautics and Astronautics (BUAA)	China
13		an experimental investigation on cowl lip's open process of two-dimensional inlet	discussion		Dr. Dinghua Feng	State Key Laboratory of Astronautic Dynamics, Xi'an Satellite Control Center	China
14		fundamental study on pulse detonation engine with liquid fuel for aerospace propulsion system	discussion		Mr. Ryuji NAKAWATASE	Kyushu University	Japan