Volume 28 Issue 5
May  2013
Turn off MathJax
Article Contents
TAO Yang, LIU Guang-yuan, ZHANG Zhao, GUO Dan-ping, LIN Jun, XIONG Neng. Engine nacelle lip design for high speed TPS wind tunnel tests[J]. Journal of Aerospace Power, 2013, 28(5): 1081-1085.
Citation: TAO Yang, LIU Guang-yuan, ZHANG Zhao, GUO Dan-ping, LIN Jun, XIONG Neng. Engine nacelle lip design for high speed TPS wind tunnel tests[J]. Journal of Aerospace Power, 2013, 28(5): 1081-1085.

Engine nacelle lip design for high speed TPS wind tunnel tests

  • Received Date: 2012-05-28
  • Publish Date: 2013-05-28
  • Computational fluid dynamics (CFD) was adopted to investigate the effects of mass flow rate difference on nacelle outer surface pressure coefficient distribution.Inverse design optimization technique was used in engine nacelle lip correction in order to adjust the turbofan propulsion simulators(TPS) outer surface pressure distribution to make it identical with that of the real engine.The engine nacelle lip inverse design method can be used in 2.4 m transonic wind tunnel to improve jet engine flow simulation test accuracy.

     

  • loading
  • [1]
    王斌,张卫民,杜绵银.大飞机机翼气动设计技术[J].航空制造技术,2010(24):53-57. WANG Bin,ZHANG Weimin,DU Mianyin.Aerodynamic design technology of large commercial aircraft wing[J].Aeronautical Manufacturing Technology,2010(24):53-57.(in Chinese)
    [2]
    Kooi W J,Kiock R,Slauerhoff J F.Tools for the experimental study of the integration of ultra-high bypass engines on transport aircraft[R].AIAA-94-2562,1994.
    [3]
    Kooi J W,Haij L D,Hegen G H.Engine simulation with turbofan propulsion simulators in the German-Dutch wind tunnels[R].AIAA 2002-2919,2002.
    [4]
    Burgsmuller W,Kooi J W,Moller K W.Accuracy requirements for high-speed test with engine simulation on transport aircraft models in the NLR-HST[R].Fort Worth,Texas:AGARD Symposium on Aerodynamic Engine/Airframe Integration for High Performance Aircraft and Missiles,2002.
    [5]
    陶洋,范召林,赵忠良.基于CFD的带控制舵导弹的动导数计算[J].航空动力学报,2010,25(1):102-106. TAO Yang,FAN Zhaolin,ZHAO Zhongliang.Predictions of dynamic damping coefficients of basic finner based on CFD[J].Journal of Aerospace Power,2010,25(1):102-106.(in Chinese)
    [6]
    Wilcox D C.A half century historical review of the k-ω model[R].AIAA-91-0615,1991.
    [7]
    Charles G,Anderson E C,Abid R.A critical evaluation of two-equation models for near wall turbulence[R].NASA CR-182068,1990.
    [8]
    Hicks R M,Henne P A.Wing design by numerical optimization[J].Journal of Aircraft,1978,15(2):58-59.
    [9]
    Dubuc L,Cantariti F,Woodgate M,et al.A grid deformation technique for unsteady flow computations[J].International Journal for Numerical Methods in Fluids,2000,32(3):285-311.
    [10]
    Morton S A,Melville R B,Visbal M R.Accuracy and coupling issues of aeroelastic Navier-Stokes solution on deforming meshes[J].Journal of Aircraft,1998,35(5):798-805.
    [11]
    Jones W T,Samareh A J.A grid generation system for multi-disciplinary design optimization[C]//12th AIAA Computational Fluid Dynamics Conference Proceedings.Washington DC:AIAA,1995:474-482.
    [12]
    Liu G Y,TAO Yang.Supercritical wing drag reduction with optimizations of 3D contour bumps[C]//Proceedings of Thirteenth Chinese Conference SSTA 2011.Huangshan:Chinese Association of Automation,2011:828-832.
    [13]
    Vanderplaats G N.Numerical optimization techniques for engineering design:with applications[M].New York:McGraw-Hill Book Company,1984:145-178.
    [14]
    Gill P E,Murray W,Wright M H.Practical optimization[M].London:Academic Press,1981:268-305.
    [15]
    Samuel K.Large-scale sequential quadratic programming algorithms[R].California:Stanford University,SOL 92-4,1992.
  • 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

    Article Metrics

    Article views (1699) PDF downloads(1008) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return