Numerical Solution of Compressible Steady Flows around the NACA 0012 Airfoil

被引：0
|
作者：
Krystufek, P. [1 ]
Kozel, K. [2 ]
机构：
[1] Tech Univ Liberec, Fac Mech Engn, Liberec, Czech Republic
[2] Czech Tech Univ, Fac Mech Engn, Prague, Czech Republic
来源：
EFM12 - EXPERIMENTAL FLUID MECHANICS 2012 | 2013年 / 45卷
关键词：
D O I：
10.1051/epjconf/20134501121
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
The article presents results of a numerical solution of subsonic and transonic flows described by the system of Navier-Stokes equations in 2D laminar compressible flows around the NACA 0012 airfoil. Authors used Runge-Kutta method to numerically solve the flows around the NACA 0012 airfoil.
引用
收藏
页数：4
相关论文
共 50 条
  • [1] Numerical Solution of Compressible Steady Flows around the RAE 2822 Airfoil
    Krystufek, P.
    Kozel, K.
    [J]. EFM13 - EXPERIMENTAL FLUID MECHANICS 2013, 2014, 67
  • [2] Numerical Solution of Inviscid Compressible Steady Flows around the RAE 2822 Airfoil
    Krystufek, P.
    Kozel, K.
    [J]. EFM14 - EXPERIMENTAL FLUID MECHANICS 2014, 2015, 92
  • [3] Computation of rarefied gas flows around a NACA 0012 airfoil
    Fan, J
    Boyd, ID
    Cai, CP
    Hennighausen, K
    Candler, GV
    [J]. AIAA JOURNAL, 2001, 39 (04) : 618 - 625
  • [4] Direct numerical simulation of flow separation around a NACA 0012 airfoil
    Shan, H
    Jiang, L
    Liu, CQ
    [J]. COMPUTERS & FLUIDS, 2005, 34 (09) : 1096 - 1114
  • [5] Large eddy simulation of unsteady, compressible, separated flow around NACA 0012 airfoil.
    Tenaud, C
    Phuoc, LT
    [J]. COMPUTATIONAL FLUID DYNAMICS '96, 1996, : 1100 - 1106
  • [6] On the Unsteady Behavior of the Flow Around NACA 0012 Airfoil with Steady External Conditions at Re=1000
    Kurtulus, Dilek Funda
    [J]. INTERNATIONAL JOURNAL OF MICRO AIR VEHICLES, 2015, 7 (03) : 301 - 326
  • [7] Computational investigation of the steady and unsteady flow field developed around a NACA0012 airfoil
    Laboratoire de Mécanique Appliquée, Faculté de Mécanique, Université des Sciences et de la Technologie d'Oran, B.P. 1505, El'mnaouar, Oran, Algeria
    [J]. International Journal of Heat and Technology, 2007, 25 (01) : 125 - 129
  • [8] Numerical Investigation of a NACA 0012 Airfoil in Oscillatory Motions
    Fu, Zhidong
    Cheng, Yongsheng
    Liu, Hong
    [J]. JOURNAL OF AIRCRAFT, 2012, 49 (06): : 2095 - 2099
  • [9] Lyapunov spectrum of the separated flow around the NACA 0012 airfoil and its dependence on numerical discretization
    Fernandez, P.
    Wang, Q.
    [J]. JOURNAL OF COMPUTATIONAL PHYSICS, 2017, 350 : 453 - 469
  • [10] Steady-state laminar flow solutions for NACA 0012 airfoil
    Swanson, R. C.
    Langer, S.
    [J]. COMPUTERS & FLUIDS, 2016, 126 : 102 - 128
12345