Showing 341 - 360 results of 1,473 for search '"Airfoil"', query time: 0.10s Refine Results
  1. 341

    Study on design characteristics of airfoil pressure distribution for low Mach number general aircraft by ZHANG Yu, BAI Junqiang, QU Feng

    Published 2023-02-01
    “…This paper studies several problems that may exist in the aerodynamic design of low Mach number general aircraft, and discusses the design characteristics of the pressure distribution of some related airfoils while part of the characteristics is verified by a multi-point laminar airfoil design case. …”
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    Article
  2. 342
  3. 343

    Aerodynamic optimization of NACA 0012 airfoils with attached Gurney flap in the rarefied gas flow by Keren Lin, Songqin Zhang, Chenfan Liu, Haiwei Yang, Bin Zhang

    Published 2023-12-01
    “…The aerodynamic optimization of a Gurney flap attached to the NACA 0012 airfoil in rarefied gas flow is studied in this study. …”
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    Article
  4. 344

    Investigation of Flow Field in Deep Dynamic Stall over an Oscillating NACA 0012 Airfoil by D. Surekha R. S., A. Khandelwal, R. Rajasekar

    Published 2019-01-01
    Subjects: “…Sinusoidal oscillation; Unsteady flow; Pitching airfoil; Numerical simulation.…”
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    Article
  5. 345

    Numerical investigation on the aerodynamic efficiency of bio-inspired corrugated and cambered airfoils in ground effect by G. R. Abdizadeh, M. Farokhinejad, S. Ghasemloo

    Published 2022-11-01
    “…Abstract This research numerically investigates the flapping motion effect on the flow around two subsonic airfoils near a ground wall. Thus far, the aerodynamic efficiency of the dragonfly-inspired flapping airfoil has not been challenged by an asymmetric cambered airfoil considering the ground effect phenomenon, especially in the MAV flight range. …”
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    Article
  6. 346

    OPTIMASI AIRFOIL MENGGUNAKAN PARTICLE SWARM DENGAN PARAMETERISASI CST (CLASS SHAPE TRANSFORMATION) by Eva Hertnacahyani Herraprastanti

    Published 2017-11-01
    “…Airfoil merupakan profil penampang yang diaplikasikan pada sarana transportasi maupun pembangkit energi sebagai penampang sudu turbin. …”
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    Article
  7. 347

    Large eddy simulation of dynamic stall over an airfoil and its control with plasma actuator by Hengyang Zhang, Haocheng Yu, Ao Zhang, Jianguo Zheng

    Published 2023-02-01
    “…The airfoil oscillates at a reduced frequency of k = 0.08 with the angle of attack (AoA) varying between 5° and 25°. …”
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  8. 348

    Aerodynamic Shape Optimization of a Symmetric Airfoil from Subsonic to Hypersonic Flight Regimes by Bernardo Leite, Frederico Afonso, Afzal Suleman

    Published 2022-11-01
    “…This work aims to optimize the aerodynamic performance of a two-dimensional baseline airfoil (NACA0012) at distinct flight regimes from subsonic to hypersonic speeds. …”
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  9. 349
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  11. 351

    Effect of Vortex Generators on Airfoil NACA 632-415 to Aerodynamic Characteristics Using CFD by Rosyida Permatasari, Gusty Widyawati

    Published 2023-02-01
    “…To determine the aircraft’s flight performance, the airfoil type must be considered when designing the wing. …”
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  12. 352
  13. 353

    Numerical simulation of flow characteristics behind the aerodynamic performances on an airfoil with leading edge protuberances by Ming Zhao, Mingming Zhang, Jianzhong Xu

    Published 2017-01-01
    “…This article presents a numerical investigation of the effects of leading-edge protuberances on airfoil stall and post-stall performance. An improved delayed detached eddy simulation (IDDES) method was adopted. …”
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    Aerodynamic design of a double slotted morphed flap airfoil– a numerical study by S. S. Shahrokhi, M. Taeibi Rahni, P. Akbari

    Published 2024-03-01
    “…The study shows that utilizing double-slotted morphing in the NACA 4412 airfoil at a 30° flap deflection angle increased the lift coefficient by 82% compared to the un-morphed state. …”
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  19. 359

    Airfoil trailing-edge noise prediction based on CFD/CAA coupled boundary method by LU Rui, DING Yongle, YU Peixun, TAN Kun, PAN Guang

    Published 2023-04-01
    “…In order to study the rationality of flow-induced noise hybrid method, the numerical simulation of acoustic radiation at the trailing edge of NACA0012 airfoil in BANC experiment was carried out. Compared with the results of sound field solved by large eddy simulation method, the analysis shows that the high-precision flow-induced noise hybrid method based on sound wave boundary conditions can predict the spatial sound field distribution with high precision and directly reflect the interaction between sound waves. …”
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  20. 360