Volume 27 Issue 8
Aug.  2012
Turn off MathJax
Article Contents
Article Navigation >  Journal of Aerospace Power  > 2012  >  27(8): 1801-1808
ZHANG Shuai, YU Xiong-qing. Model of open rotor engine for aircraft conceptual design[J]. Journal of Aerospace Power, 2012, 27(8): 1801-1808.
Citation: ZHANG Shuai, YU Xiong-qing. Model of open rotor engine for aircraft conceptual design[J]. Journal of Aerospace Power, 2012, 27(8): 1801-1808.
shu

Model of open rotor engine for aircraft conceptual design

  • Key Laboratory of Fundamental Science for National Defense-Advanced Design Technology of Flight Vehicle,College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China

  • Received Date: 2011-09-19
  • Publish Date: 2012-08-28
    Abstract
  • A rapid analysis model of the open rotor engine,which can be used in aircraft conceptual design,was established by the combination of the test data of high speed propfan and approximate model of turboshaft.The performance,mass and size of the open rotor engine were able to be predicted quickly by this model with a small amount of input parameters.The precision of the model was validated by the experimental data from the references.The model developed in the paper can be used in the aircraft conceptual design to evaluate the benefits of using open rotor engines.

     

    • FullText(HTML)
  • loading
    • References(12)
  • [1]
    胡晓煜.下一代窄体客机发动机最新进展[J].航空发动机,2010,36(1):52-56. HU Xiaoyu.Latest development of next generation narrow aircraft engine[J].Aeroengine,2010,36(1):52-56.(in Chinese)
    [2]
    Awker R W.Evaluation of propfan propulsion applied to general aviation .NASA CR-175020,1986.
    [3]
    Parzyeh D,Shenkman A,Cohen S.Large scale advanced prop-fan (LAP) performance,acoustic and weight estimation .NASA CR-174782,1984.
    [4]
    Jackson A J B.Optimisation of aero and industrial gas turbine design for the environment .Cranfield,UK:Cranfield University,2009.
    [5]
    Bellocq P,Sethi V,Cerasi L,et al.Advanced open rotor performance modelling for multidisciplinary optimization assessments .ASME GT-2010-22963,2010.
    [6]
    Smith N R,Blessing B,Dixon J,et al.Conceptual design of an environmentally responsible 150-passenger commercial aircraft .AIAA 2010-1392,2010.
    [7]
    Baum J A,Dumais P J,Mayo M G,et al.Prop-fan data support study .NASA CR-152141,1978.
    [8]
    Jeracki R J,Mikkelson D C,Blaha B J.Wind tunnel performance of four energy efficient propellers designed for Mach 0.8 cruise .NASA TM-79124,1979.
    [9]
    Howe D.Aircraft conceptual design synthesis[M].London,Bury St Edmunds:Professional Engineering Publishing Limited,2000.
    [10]
    尚义.航空燃气涡轮发动机[M].北京:航空工业出版社,1995.
    [11]
    Jenkinson L R,Simpkin P,Rhodes D.Civil jet aircraft design[M].London:Arnold (a Member of the Hodder Headline Group),1999.
    [12]
    GE Aircraft Engines GE36 Project Department.Full scale technology demonstration of a modern counterrotating unducted fan engine concept .NASA CR-180867,1987.
    • Relative Articles
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF(566.0KB)
    XML

    Article Metrics

    Article views (1811) PDF downloads(562) Cited by()
    Proportional views
    Related

    Copyright © 《Journal of Aerospace Power》 All Rights Reserved.

    Supported by: Beijing Renhe Information Technology Co., Ltd.  

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return