IAF Digital Library

9

session 9

Title: Hypersonic and Combined Cycle Propulsion
type: oral
Description: This session covers papers on Hypersonic and Combined Cycle Propulsion for space applications.
Date: 2016-09-27
Time: 14:45
Room: Zapopan

IPC members

Co-Chair: Dr. Helen Webber, Reaction Engines Ltd., United Kingdom;
Co-Chair: Prof. Riheng Zheng, Beihang University, China;
Rapporteur: Dr. Salvatore Borrelli, CIRA Italian Aerospace Research Centre, Italy;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		KEYNOTE: Shock Tunnel Development for Air-breathing Propulsion Testing at True Hypersonic Flight Conditions	30'	confirmed	Mr. Zonglin Juang	Institute of Mechanics, Chinese Academy of Sciences	China
2		SABRE Technology Development	15'	confirmed	Dr. Helen Webber	Reaction Engines Ltd.	United Kingdom
3		research on aerodynamic performance of a typical hypersonic inwardturning inlet	15'	confirmed	Dr. Dawei Yang		China
3		research on aerodynamic performance of a typical hypersonic inwardturning inlet	15'	confirmed	Prof. Anyuan YU	China Aerodynamics Research and Development Center (CARDC)	China
4		Preliminary Design and Performance Studies of a Wide Range Rocket-based Combined Cycle Engine	15'	confirmed	Dr. Feiteng Luo	Science and Technology on Scramjet Laboratory, Beijing Power Machinery Research Institute	China
5		Development of an integrated platform for scramjet engine optimization design	15'	confirmed	Mr. yuanguang wang	Beijing Electro-Mechanical Engineering Institute, China Aerospace Science & Industry Corporation (CASIC)	China
6		research on shock train leading edge detection in scramjet	15'	confirmed	Mr. Chengyi Su	Science and Technology on Scramjet Laboratory, Beijing Power Machinery Research Institute	China
7		The Research of Air-Turbo-Rocket (ATR) Propulsion System Based on Double Solid Propellant Gas-Generator	15'	withdrawn	Dr. yang LIU	Science and Technology on Combustion, Internal Flow and Thermal-structure Laboratory, Northwestern Polytechnical University	China
8		A Pre-cooled and Fuel-rich Pre-burned Mixed-flow Turbofan Cycle for Ground-to-Ma5 Engines	15'	withdrawn	Dr. Wei Zhao	Chinese Academy of Sciences	China
9		Investigation of an Air Turborocket based Propulsion System	15'	confirmed	Dr. Yen-Sen Chen	American Institute of Aeronautics and Astronautics (AIAA)	Taiwan, China
10		LIFE EVALUATION OF REUSABLE RAMJET ENGINE SUBJECTED TO CREEP-FATIGUE INTERACTION	15'	withdrawn	Ms. Lili Fu	School of Astronautics,Northwestern Polytechnical University	China
11		mixing enhancement using secondary gas ejection method in supersonic-subsonic shear layer	15'	withdrawn	Mr. Chenxi Zhang	Northwestern Polytechnical University,NPU	China
12		A Parallel Direct-Connect Test System for Solid Ducted Rocket	15'	confirmed	Mr. Jiming Cheng	Science and Technology on Combustion, Internal Flow and Thermal-structure Laboratory,Northwestern Polytechnical University	China
13		Multi-Points Integrated Airframe/Engine Configuration Optimization of Hypersonic Vehicle	15'	withdrawn	Ms. Qing Wang	College of Mechanical and Electrical Engineering, Xi'an Polytechnic University	China
14		airframe-propulsion integrated design and wind tunnel test for air-breathing hypersonic vehicle	15'	confirmed	Mr. Zi-han Jiao	China Academy of Launch Vehicle Technology (CALT)	China
15		Performance evaluation and the status of TRRE	15'	confirmed	Dr. Wenhui Ling	Science and Technology on Scramjet Laboratory, Beijing Power Machinery Research Institute	China
16		Design of Liquid Propellant Supply System with Wide Regulation Range of Primary Rocket in Rocket-Based Combined Cycle (RBCC) engine	15'	withdrawn	Ms. Jingjing Bai		China