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  • 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: Dr. Riheng Zheng, China Aerospace Science & Industry Corporation (CASIC), China;

    • Rapporteur: Dr. Salvatore Borrelli, CIRA Italian Aerospace Research Centre, Italy;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    14:45

    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

    15:00

    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    withdrawn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

    15:15

    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 (NPU)

    China

    4

    15:30

    study of the thermal adjustment of rbcc based on two-stage injections

    15'

    confirmed

    Mr. Ya Jun Wang

    College of Astronautics, Northwestern Polytechnical University (NPU)

    China

    5

    15:45

    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

    16:00

    Precooler development and performance analysis of a precooling air turbo rocket engine

    15'

    withdrawn

    Mr. LI Wenlong

    Xi'an Aerospace Propulsion Institute

    China

    8

    16:15

    Investigation of the propellant proheating in air turbo rocket engine

    15'

    confirmed

    Mr. LI Wenlong

    Xi'an Aerospace Propulsion Institute

    China

    9

    16:30

    detonation combustion wave stabilization in scramjets

    15'

    withdrawn

    Mr. Ryan Clark

    United States

    10

    16:45

    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

    17:00

    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

    17:15

    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

    17:30

    study on the turbo-pump performance of the scramjet fuel feed system

    15'

    confirmed

    Prof. Shen Chibing

    National University of Defense Technology

    China

    14

    17:45

    Experimental and Numerical Investigation of Flow Reaction and Heat Transfer with Supercritical Hydrocarbon Fuel

    15'

    withdrawn

    Mr. Zhao Yunlong

    China