Numerical analysis of transport aircraft using different wing tip devices

被引：0
|
作者：
Streit, Th. [1 ]
Ronzheimer, A. [1 ]
Buescher, A. [2 ]
机构：
[1] DLR, Inst Aerodynam & Flow Technol, Lilienthalpl 7, D-38108 Braunschweig, Germany
[2] Braunschweig Tech Univ, Inst Fluid Mech, D-38106 Braunschweig, Germany
来源：
NEW RESULTS IN NUMERICAL AND EXPERIMENTAL FLUID MECHANICS V | 2006年 / 92卷
关键词：
D O I：
10.1007/978-3-540-33287-9_8
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Numerical solutions of the Navier Stokes equations for a modem transport configuration with three different wing tip devices are presented. Solutions are obtained at high speed for the cruise configuration and at low speed for the corresponding take-off configuration. This study is performed within the European Union project M-DAW (Modelling and Design of Advanced Wing Tip Devices). The numerical results are analysed to characterise the performance of the wing tip devices using global force coefficients, local distributions of force and moment, surface contours and skin friction lines. In addition the vortex wake was analysed in the near field tip region for take-off. Numerical results are compared with experimental data obtained in cryogenic wind tunnel tests at high speed in the ETW (European Transonic Wind tunnel) and at low speed in the DNW-KKK (Cryogenic Wind Tunnel Cologne).
引用
收藏
页码：59 / +
页数：3
相关论文
共 50 条
  • [21] TRANSONIC WING DESIGN FOR TRANSPORT AIRCRAFT.
    Krenz, Guenter
    Prace Instytutu Metalurgii Zelaza im St. Staszica, 1979, : 52 - 61
  • [22] Aerodynamic Optimization Study on Transport Aircraft Wing
    Darshan, Y. N.
    Narahari, H. K.
    Sriram, A. T.
    ADVANCED TRENDS IN MECHANICAL AND AEROSPACE ENGINEERING (ATMA-2019), 2021, 2316
  • [23] Aerodynamic optimisation of a flying wing transport aircraft
    Strueber, H.
    Hepperle, M.
    NEW RESULTS IN NUMERICAL AND EXPERIMENTAL FLUID MECHANICS V, 2006, 92 : 69 - +
  • [24] Aerodynamic Wing Design for Transport Aircraft - Today
    Horstmann, K. H.
    Streit, T.
    HERMANN SCHLICHTING - 100 YEARS, 2009, 102 : 130 - 144
  • [25] Numerical Investigation of Wingtip Vortex Attenuation Using a Tip-Chipped Wing
    Roh, Nahyeon
    Oh, Sejong
    Yee, Kwanjung
    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2017, 60 (04) : 244 - 254
  • [26] VARIABLE WING CAMBER FOR TRANSPORT AIRCRAFT.
    Szodruch, J.
    Hilbig, R.
    Progress in Aerospace Sciences, 1988, 25 (03) : 297 - 328
  • [27] Numerical analysis of propeller effects on wing aerodynamic: tip mounted and distributed propulsion
    Della Vecchia, Pierluigi
    Malgieri, Daniele
    Nicolosi, Fabrizio
    De Marco, Agostino
    AEROSPACE EUROPE CEAS 2017 CONFERENCE, 2018, 29 : 106 - 115
  • [28] Transport aircraft three-dimensional high-lift-wing numerical transition prediction
    Perraud, J.
    Cliquet, J.
    Houdeville, R.
    Arnal, D.
    Moens, F.
    Journal of Aircraft, 1600, 45 (05): : 1554 - 1563
  • [29] Transport Aircraft Three-Dimensional High-Lift-Wing Numerical Transition Prediction
    Perraud, J.
    Cliquet, J.
    Houdeville, R.
    Arnal, D.
    Moens, F.
    JOURNAL OF AIRCRAFT, 2008, 45 (05): : 1554 - 1563
  • [30] Numerical study of fatigue damage accumulation in composite wing panels of prospective supersonic transport aircraft
    Turbin N.V.
    Shelkov K.A.
    Aerospace Systems, 2023, 6 (03) : 481 - 490
12345