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  • session 9

    Title

    Hypersonic and Combined Cycle Propulsion

    Description

    This session covers papers on space propulsion application and R&D with a wide range of interest.

    Date

    2013-09-24

    Time

    14:45

    Room

    208A

    IPC members
    • Chairman: Dr. Salvatore Borrelli, CIRA Italian Aerospace Research Centre, Italy;

    • Chairman: Prof. Shigeru Aso, Kyushu University, Japan;

    • Rapporteur: Mr. Patrick Danous, ArianeGroup, France;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Combined Cycle Propulsion System?Challenge and Prospects

    15'

    confirmed

    Mr. zhang chengzhi

    China Academy of Launch Vehicle Technology (CALT)

    China

    2

    Computational Investigation of effect of Converging-Diverging Nozzle (C-D Nozzle) on the Performance of Pulse Detonation Engine(PDE)- Effects on Thrust and Inlet Pressure

    15'

    Dr. Ugur Guven

    United States

    3

    Comprehensive Consideration of Gelled fuel in hypersonic ramjet propulsion

    15'

    withdrawn

    Dr. Jianxin HU

    China

    4

    The constant pressure time in a piston driver of free piston shock tunnel

    15'

    Dr. Zhu Hao

    China Academy of Aerospace Aerodynamics (CAAA)

    China

    5

    experimental study on rbcc with oxygen/kerosene firstly combustion

    15'

    confirmed

    Dr. Liang Tian

    Beihang University

    China

    6

    Measurements of two-dimensional temperature distribution in combustion using diode laser absorption spectroscopy

    15'

    confirmed

    Dr. Junling Song

    Academy of Equipment

    China

    7

    Influencing Factors on the Mode Transition in a Dual-Mode Scramjet Combustor

    15'

    confirmed

    Mr. zhang yan

    Beihang University

    China

    8

    Mixing and combustion characteristics with lobe nozzel upstream of a V-gutter in a subsonic flow

    15'

    withdrawn

    Ms. yanan Wang

    National University of Defense Technology

    China

    9

    System Design and Analysis of Hydrocarbon Scramjet with Regeneration Cooling and Expansion Cycle

    15'

    Dr. Wu Xianyu

    College of Aerospace and Materials Engineering, National University of Defense Technology

    China

    10

    CALCULATION OF AERODYNAMIC CHARACTERISTICS OF SAME MODEL SWIVEL NOZZLES WITH MATHEMATICAL MODELING OF REAL GAS EFFECTS

    15'

    confirmed

    Dr. Alexey Galaktionov

    Central Research Institute for Machine Building (FGUP TSNIIMASH)

    Russian Federation

    11

    Thermodynamic limitation on boron energy realization in ramjet propulsion

    15'

    confirmed

    Prof. Alon Gany

    TECHNION - Israel Institute of Technology

    Israel

    12

    Thermal decomposition of model endothermic hydrocarbon fuels and their mixtures

    15'

    confirmed

    Dr. Rongpei Jiang

    Beijing institute of aerospace testing technology

    China

    13

    Experimental Investigation on Angled Transverse Liquid Jet in Supersonic Crossflow

    15'

    confirmed

    Mr. Tong Yiheng

    College of Aerospace and Materials Engineering, National University of Defense Technology

    China