session 7

Title: Hypersonic Air-breathing and Combined Cycle Propulsion, and Hypersonic Vehicle
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, detonation 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, together with the associated vehicle.
Date: 2025-10-02
Time: 10:15
Room: Room C3.6

IPC members

Co-Chair: Dr. Yen-Sen Chen, American Institute of Aeronautics and Astronautics (AIAA), United States;
Co-Chair: Prof. Riheng Zheng, Beihang University, China;
Rapporteur: Dr. Lahib Balika, Thales Alenia Space, United Kingdom;
Rapporteur: Mr. Didier Boury, ArianeGroup SAS, France;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	10:15	Air Turbo Engine Gas Generator for Vertical Take-off and Landing Demonstrator Vehicle	12		Dr. Yuki Sakamoto	Japan Aerospace Exploration Agency (JAXA), ISAS	Japan
2	10:27	Combustion characteristics of liquid kerosene in a scramjet combustor with strut-cavity flameholder	12		Mr. jingyu zhang		China
3	10:39	Combustion performance and cooling/drag reduction characteristics of supersonic film cooling using fuel as coolant	12		Dr. Jingying Zuo	Harbin Institute of Technology	China
4	10:51	Study of Fuel-Oxidiser Mixture and Detonation Wave Dynamics for Rotation Detonation Engine	12		Mr. Abishek Shrestha		Australia
5	11:03	Critical Criterion Modeling of Local Flame Generation and Global Flame Establishment in Large-Scale Scramjet Combustor using Torch Ignition	12		Dr. Mengcheng Yuan	Northwestern Polytechnical University	China
6	11:15	imaging and characterisation of shear layer instabilities in transverse jets in supersonic crossflow	12		Mr. Erik Mueller	UNSW Australia	Australia
7	11:27	Effects of Contaminated Heating Component on the Ignition and Combustion of Ramjet Engine in Direct-Connect Tests	12		Ms. Xue Yang	Northwestern Polytechnical University	China
8	11:39	Revolutionary Turbine Based Combined Cycle (TBCC) Ramjet Design for Hypersonic Space Access Vehicles	12		Mr. Jimit Pathak	Vellore Institute of Technology	India
9	11:51	Optimized Aircraft Geometry for Hypersonic Flow: CFD and Thermal Integration of Hydrogen-Powered Scramjet engine	12	confirmed	Mr. Marco Cárdenas Aldaco	Administración de Sistemas Aeroespaciales Mexicanos - ASAEM	Mexico
10	12:03	experimental study on functional verification of heat-resistant and insulation systems for air turbo rocket engine secondary combustors	12		Mr. Motoki Ida	The Graduate Universty for Advanced Studies[SOKENDAI]	Japan
11	12:15	Design and Testing of a Ramjet as a Second Stage for Small Scale Rocket Models	12		Dr. Francesco Margani	GAUSS S.r.l.	Italy
12	12:27	HYBRID ROTATING DETONATION ROCKET ENGINE WITH INTEGRATED THERMAL BUFFERING FOR ENHANCED EFFICIENCY AND DURABILITY	12		Ms. Kavya Dichwalkar	VIT Bhopal University	India
13*	12:39	inlet-engine matching control of rocket based combined cycle engine under rocket-ramjet mode	12	confirmed	Dr. Wenhui Ma	College of Astronautics, Northwestern Polytechnical University	China
14*	12:39	Aerodynamic Configuration Design and Simulation Analysis of Baffle-Type Fairings	12		Dr. Hua Zhang	Jiuquan Satellite Launch Center	China
15*	12:39	Validation of Computationally Efficient CFD Models for Flow Field Analysis in Hypersonic Engines	12		Mr. Kei Fukuzawa	Kanazawa Institute of Technology	Japan
16*	12:39	Solid Ramjet Gas Generator Fuel: Additive Effects and Altitude Performance Analysis	12		Mr. Abdul Rahman	Scuola di Ingegneria Aerospaziale "La Sapienza"	Italy
17*	12:39	geometrical structure design and optimization on an air-augmented solid rocket combustor	12		Mr. Zhaoyang Tian	Northwestern Polytechnical University	China
18*	12:39	A review on characteristic of Scramjet Combustor based on fuel selection	12		Ms. Srishti Bansal	Space Generation Advisory Council (SGAC)	India

session 7

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