Roughness effects on heat transfer from a NACA 0012 airfoil

被引：0
|
作者：
机构：
[1] Poinsatte, Philip E.
[2] Van Fossen, G.James
[3] De Witt, Kenneth J.
来源：
Poinsatte, Philip E. | 1600年 / 28期
基金：
美国国家航空航天局;
关键词：
Aerodynamics--Wings and Airfoils - Heat Transfer - Surfaces;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
相关论文
共 50 条
  • [41] Finite Element Solutions for Turbulent Flow over the NACA 0012 Airfoil
    Anderson, W. Kyle
    Ahrabi, Behzad R.
    Newman, James C.
    AIAA JOURNAL, 2016, 54 (09) : 2688 - 2704
  • [42] Simulation of dynamic stall for a NACA 0012 airfoil using a vortex method
    Akbari, MH
    Price, SJ
    JOURNAL OF FLUIDS AND STRUCTURES, 2003, 17 (06) : 855 - 874
  • [43] AERODYNAMIC CHARACTERISTICS OF NACA 0012 AIRFOIL IN RELATION TO WIND GENERATORS.
    Michos, A.
    Bergeles, G.
    Athanassiadis, N.
    Wind Engineering, 1983, 7 (04) : 247 - 262
  • [44] Study on the effect of raindrops on the dynamic stall of a NACA-0012 airfoil
    Sheidani, Armin
    Salavatidezfouli, Sajad
    Schito, Paolo
    JOURNAL OF THE BRAZILIAN SOCIETY OF MECHANICAL SCIENCES AND ENGINEERING, 2022, 44 (05)
  • [45] Study on the effect of raindrops on the dynamic stall of a NACA-0012 airfoil
    Armin Sheidani
    Sajad Salavatidezfouli
    Paolo Schito
    Journal of the Brazilian Society of Mechanical Sciences and Engineering, 2022, 44
  • [46] The solution of unsteady inverse problem for NACA-65-0012 airfoil
    University of Shanghai for Science and Technology, Shanghai 200093, China
    不详
    Kung Cheng Je Wu Li Hsueh Pao, 2006, 6 (947-949):
  • [47] EXPERIMENTAL AERODYNAMIC CHARACTERISTICS OF AN NACA-0012 AIRFOIL WITH SIMULATED ICE
    KORKAN, KD
    CROSS, EJ
    CORNELL, CC
    JOURNAL OF AIRCRAFT, 1985, 22 (02): : 130 - 134
  • [48] Aeroelastic dynamics of a NACA 0012 airfoil in the transitional Reynolds number regime
    Poirel, Dominique
    Harris, Yael
    Benaissa, Azemi
    PROCEEDINGS OF THE ASME PRESSURE VESSELS AND PIPING CONFERENCE VOL 9, 2007, : 847 - 854
  • [49] Unsteady aerodynamics of a pitching NACA 0012 airfoil at low Reynolds number
    Kurtulus, Dilek Funda
    INTERNATIONAL JOURNAL OF MICRO AIR VEHICLES, 2019, 11
  • [50] The Effects Of NACA 0012 Airfoil Modification on Aerodynamic Performance Improvement and Obtaining High Lift Coefficient and Post-Stall Airfoil
    Sogukpinar, Haci
    TURKISH PHYSICAL SOCIETY 33RD INTERNATIONAL PHYSICS CONGRESS (TPS33), 2018, 1935
12345