IAF Digital Library

9

session 9

Title: Hypersonic and Combined Cycle Propulsion
Description: This session covers papers on Hypersonic and Combined Cycle Propulsion for space applications.
Date: 2015-10-13
Time: 14:45
Room: Ballroom B (Crowne Plaza Hotel, -1 floor)

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		Numerical and Experimental Studies of Flame Stabilization in a Cavity Stabilized RBCC Combustor	15'	confirmed	Mr. LI Wenlong	Xi'an Aerospace Propulsion Institute	China
2		The supersonic waverider aerodynamic configuration with Rocket Based Combined Cycle(RBCC)engine aerodynamic/propulsion integration	15'	withdrawn	Dr. Yi Li	China Academy of Launch Vehicle Technology(CALT)	China
3		effects of primary rocket nozzle expansion ratio on combustion oscillating characteristics in a rbcc engine combustor	15'	confirmed	Mr. Ya Jun Wang	College of Astronautics, Northwestern Polytechnical University	China
4		study of the thermal adjustment of rbcc based on two-stage injections	15'	confirmed	Mr. Ya Jun Wang	College of Astronautics, Northwestern Polytechnical University	China
5		A Novel Turbo-aided Rocket-augmented Ramjet Combined Cycle Engine Concept	15'	confirmed	Dr. Baoxi Wei	Science and Technology on Scramjet Laboratory, Beijing Power Machinery Research Institute	China
7		Precooler development and performance analysis of a precooling air turbo rocket engine	15'	withdrawn	Mr. LI Wenlong	Xi'an Aerospace Propulsion Institute	China
8		Investigation of the propellant proheating in air turbo rocket engine	15'	confirmed	Mr. LI Wenlong	Xi'an Aerospace Propulsion Institute	China
9		detonation combustion wave stabilization in scramjets	15'	withdrawn	Mr. Ryan Clark		United States
10		Numerical study on mixing of a passive scalar in supersonic mixing layers using a hybrid RANS/LES approach	15'	confirmed	Dr. Junhong Feng	Science and Technology on Scramjet Laboratory, National University of Defense Technology	China
11		Cowl and Cavity Effects on Scramjet Fuel Mixing and Combustion	15'	withdrawn	Mr. Won Keun Chang	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
12		real time estimation of air mass flow rate for scramjet inlet based on multi-sensor fusion	15'	confirmed	Mr. Chengyi Su	Science and Technology on Scramjet Laboratory, Beijing Power Machinery Research Institute	China
13		study on the turbo-pump performance of the scramjet fuel feed system	15'	confirmed	Prof. Shen Chibing	National University of Defense Technology	China
14		Experimental and Numerical Investigation of Flow Reaction and Heat Transfer with Supercritical Hydrocarbon Fuel	15'	withdrawn	Mr. Zhao Yunlong		China