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  • 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

    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    withdrawn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

    Mr. Qiang Gang

    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    withdrawn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    withdrawn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