session 9
- Title
Hypersonic Air-breathing and Combined Cycle Propulsion
- type
oral
- Description
This session covers hypersonic air-breathing and combined cycle propulsion with space applications. The typical types of engine considered in this session include: turbojet, ramjet, Scramjet, denotation engine, Turbine Based Combined Cycle (TBCC), Rocket Based Combined Cycle (RBCC), Hypersonic Pre-cooled Propulsion, Air Turbo Rocket (ATR) and other types of hypersonic combined cycle propulsion.
- Date
2017-09-26
- Time
- Room
- IPC members
Co-Chair: Prof. Riheng Zheng, Beihang University, China;
Co-Chair: Dr. Helen Webber, Reaction Engines Ltd., United Kingdom;
Rapporteur: Dr. Salvatore Borrelli, CIRA Italian Aerospace Research Centre, Italy;
Order | Time | Paper title | Mode | Presentation status | Speaker | Affiliation | Country |
|---|---|---|---|---|---|---|---|
1 | 14:45 | analysis on the performance of a hypersonic inward turning inlet with three combined channels | 10 | confirmed | Dr. Chengxiang Zhu | Xiamen University | China |
2 | 14:55 | 10 | no-show | Mr. ren jiawan | China | ||
3 | 15:05 | Development of optical diagnostics for the characterization of high-velocity combustion | 10 | confirmed | Mr. Owen Pryor | University of Central Florida (UCF) | United States |
4 | 15:15 | A Pre-cooled and Fuel-rich Pre-burned Mixed-flow Turbofan Cycle for Ground-to-Ma5 Engines | 10 | confirmed | Dr. Wei Zhao | Chinese Academy of Sciences | China |
5 | 15:25 | Thermodynamic Analysis of Helium System Cycle for the Precooled Air-breathing Combined Engine | 10 | no-show | Dr. Yuan Ma | Xi'an Aerospace Propulsion Institute | China |
6 | 15:35 | Successful Flight Testing of Scramjet Engine Over Wide Range of Test Conditions | 10' | confirmed | Mr. Lazar T. Chitilappilly | Vikram Sarabhai Space Centre (VSSC) | |
7 | 15:45 | An efficient approach for tomographic reconstruction in combustion diagnostics | 10 | confirmed | Dr. Junling Song | Equipment Academy | China |
8 | 15:55 | 10 | withdrawn | Dr. YANG LIU | China | ||
9 | 16:05 | Researches on Rocket-Based Combined-Cycle Inlet in Northwestern Polytechnical University | 10 | withdrawn | Dr. Lei Shi | Northwestern Polytechnical University，NPU | China |
10 | 16:15 | Performance Optimization Method of Turbocharged Solid Propellant Ramjet(TSPR) | 10 | confirmed | Dr. Wei Wang | 1. Systems Engineering Institute of Sichuan Aerospace; 2.Science and Technology on Combustion, Internal Flow and Thermal-Structure Laboratory, Northwestern Polytechnical University | China |
11 | 16:25 | a novel liquid rocket-ramjet combined-cycle engine enhanced by a compact internal air turborocket | 10 | confirmed | Dr. Duo Zhang | Northwestern Polytechnical University | China |
12 | 16:35 | Numerical investigation on the full flowpath performance of RBCC engine | 10 | withdrawn | Mr. Ya Jun Wang | College of Astronautics, Northwestern Polytechnical University | China |
13 | 16:45 | 10 | confirmed | Dr. Fei XING | Xiamen University | China | |
14 | 16:55 | Cycle analysis and optimization of the precooled Air Turbo-Ramjet | 10 | withdrawn | Prof.Dr. Jiang Qin | Harbin Institute of Technology | China |
15 | 17:05 | 10 | confirmed | Mr. Philipp Klink | RMIT University (Royal Melbourne Institute of Technology) | Australia | |
16 | 17:15 | Performance of High Mach Number Scramjets - Tunnel vs Flight | 10 | confirmed | Mr. Will Landsberg | University of Queensland | Australia |
17 | 17:25 | Modeling Scramjet Supersonic Combustion via Eddy Dissipation Model | 10 | confirmed | Mr. Jimmy-John Hoste | University of Strathclyde | United Kingdom |
18 | 17:35 | 10 | withdrawn | Dr. Wenhui Ling | Science and Technology on Scramjet Laboratory, Beijing Power Machinery Research Institute | China | |
19 | 17:45 | experimental research on behavior of a non-premixed rotating detonation engine | 10 | withdrawn | Dr. Yu YAN | Xi'an aerospace propulsion institure | China |