Numerical Investigation of Powered High-Lift Model with Externally Blown Flap

被引:9
|
作者
Li Jie [1 ]
Gong Zhibin [1 ]
Zhang Heng [1 ]
Jin Jing [1 ]
机构
[1] Northwestern Polytech Univ, Dept Fluid Mech, Sch Aeronaut, Xian 710072, Shaanxi, Peoples R China
来源
JOURNAL OF AIRCRAFT | 2017年 / 54卷 / 04期
基金
中国国家自然科学基金;
关键词
TRANSPORT AIRCRAFT; ENGINE; FLOW;
D O I
10.2514/1.C034270
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The externally blown flap is an approach of powered-lift technology utilizing conventional pod-mounted engines to blow exhaust over the flap surfaces. Based upon multiblock structured grid techniques and three-dimensional Reynolds-averaged Navier-Stokes computational methods, a powered high-lift principle model with externally blown flap is constructed for analysis. Different influencing factors, including engine position, engine-exhaust condition, flap deflection, and flap gap, are investigated in detail to improve powered high-lift effects. Then, flow-control techniques, such as the cove tab and downward deflection of the spoiler, are studied. The cove tab can be helpful for longitude-trim and stability problems, whereas the spoiler downward deflection can help increase lift-to-drag ratios. Both the cove tab and spoiler downward deflection can contribute to the augmentation of the lift coefficients and the elimination of the flow separation over the flap, as well as the reduction of jet-flow spanwise spreading on the leading edge of the lower flap.
引用
收藏
页码:1539 / 1551
页数:13
相关论文
共 50 条
  • [1] Method for evaluating powered high-lift effects of externally blown flap
    Zhang S.
    Wang W.
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2017, 38 (06):
  • [2] EXTERNALLY-BLOWN JET FLAP - POWERED-LIFT CONCEPT FOR STOL
    WICKENS, RH
    CANADIAN AERONAUTICS AND SPACE JOURNAL, 1974, 20 (07): : 323 - 340
  • [3] Numerical investigation of the influence of engine positions on powered high-lift effects for large transport aircraft
    College of Aeronautics, Northwestern Polytechnical University, Xi'an
    710072, China
    不详
    710065, China
    Xibei Gongye Daxue Xuebao, 4 (560-565):
  • [4] Numerical investigation of slat and compressibility effects for a high-lift wing
    Baker, MD
    Mathias, DL
    Roth, KR
    Cummings, RM
    JOURNAL OF AIRCRAFT, 2002, 39 (05): : 876 - 884
  • [5] Numerical Investigation of CL,max Prediction on the NASA High-Lift Common Research Model
    Browne, Oliver M. F.
    Housman, Jeffrey A.
    Kenway, Gaetan K.
    Ghate, Aditya S.
    Kiris, Cetin C.
    AIAA JOURNAL, 2023, 61 (04) : 1639 - 1658
  • [6] Numerical Investigation of High-Lift Propeller Positions for a Distributed Propulsion System
    Beckers, Mario Firnhaber
    Schollenberger, Michael
    Lutz, Thorsten
    Bongen, Dustin
    Radespiel, Rolf
    Florenciano, Juan L.
    Funes-Sebastian, David E.
    JOURNAL OF AIRCRAFT, 2023, 60 (04): : 995 - 1006
  • [7] Numerical investigation of secondary flows in a high-lift low pressure turbine
    Cui, J.
    Rao, V. Nagabhushana
    Tucker, P. G.
    PROCEEDINGS OF THE EIGHTH INTERNATIONAL SYMPOSIUM ON TURBULENCE HEAT AND MASS TRANSFER (THMT-15), 2015, : 847 - 850
  • [8] Numerical investigation of secondary flows in a high-lift low pressure turbine
    Cui, J.
    Rao, V. Nagabhushana
    Tucker, P. G.
    INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW, 2017, 63 : 149 - 157
  • [9] BASIC INVESTIGATION ON AN UNSWEPT RECTANGULAR WING WITH AN EXTERNALLY BLOWN FLAP
    KUEHL, P
    WELTE, D
    AIRCRAFT ENGINEERING, 1971, 43 (12): : 12 - &
  • [10] Multidisciplinary Design of an Electrically Powered High-Lift System
    Maroldt, Niklas
    Lohse, Stefanie
    Kalla, Matthias
    Ponick, Bernd
    Seume, Joerg R.
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2023, 145 (10):