位置：成果数据库 > 会议 > 会议详情页
A modular RANS approach for modeling hypersonic flow transition on an air-breathing configuration
  • 所属机构名称：清华大学
  • 会议名称：51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013
  • 时间：2013
  • 成果类型：会议
  • 相关项目：尺度自适应模拟基本起落架部件干扰机理
作者： Xiao Lianghua|Wang Liang|Xiao Zhixiang|Fu Song|
同会议论文项目
尺度自适应模拟基本起落架部件干扰机理
期刊论文 7 会议论文 23
同项目会议论文
Prediction of massive separation around landing-gear-like geometries
Unsteady flows around tandem cylinders with critical spacing
Numerical Prediction of Massive separation Unsteady Flows around Bluff-bodies
Effects of quasi-laminar hypothesis on the massive separation and unsteady flows around tandem cylin
Comparisons of three improved DES methods on unsteady flows past tandem cylinders
起落架类非定常大范围分离流动预测
Unsteady Flow Around Two Tandem Cylinders Using Advanced Turbulence Modeling Method
IDDES方法在LAST实验室的应用概况及展望
Studies of roughness-induced transition using three-quation κ-ω-γ transition/turbu
高超声速边界层内不规则表面转捩初探
Numerical investigation of shock buffet on an oat15a airfoil and control effects of vortex generator
Numerical investigations of massively separated flows past Rudimentary Landing Gear using SST-DDES
Numerical investigation of massively separated flows past RLG using advanced DES approaches
Numerical simulations of the near-field flows past cylinders in tandem arrangements
Numerical simulations of tandem cylinders with subcritical spacing
Direct numerical simulation of hypersonic transition induced by a cylindrical roughness element
RANS/LES混合方法及其应用
Simulation of transition triggered by isolated roughness in hypersonic boundary layer
Evaluation of Numerical Dissipation Sensitivity Using IDDES
Investigation of Passive Flow Control Methodologies Using IDDES
先进DES方法预测基本起落架大范围分离流动
Study into Effects of Vortex Generators on a Supercritical Wing