Three-Dimensional Modeling Shock-Wave Interaction with a Fin at Mach 5

[1]  A. Pasha Study of Parameters Affecting Separation Bubble Size in High Speed Flows using k-ω Turbulence Model , 2018 .

[2]  K. Sinha,et al.  Variable turbulent Prandtl number model for shock/boundary-layer interaction , 2017 .

[3]  Lipeng Lu,et al.  Investigation of the Three-Dimensional Shock- Wave/Turbulent-Boundary-Layer Interaction Initiated by a Single-Fin , 2016 .

[4]  K. Sinha,et al.  MODELLING OF TURBULENT ENERGY FLUX IN CANONICAL SHOCK-TURBULENCE INTERACTION , 2016, Proceeding of Ninth International Symposium on Turbulence and Shear Flow Phenomena.

[5]  J. Larsson,et al.  Turbulent energy flux generated by shock/homogeneous-turbulence interaction , 2015, Journal of Fluid Mechanics.

[6]  A. Panaras Turbulence Modeling of Flows with Extensive Crossflow Separation , 2015 .

[7]  Yang Zhiyin,et al.  Large-eddy simulation: Past, present and the future , 2015 .

[8]  Holger Babinsky,et al.  Shock Wave-Boundary-Layer Interactions , 2014 .

[9]  Jian Fang,et al.  A study on turbulence transportation and modification of Spalart–Allmaras model for shock-wave/turbulent boundary layer interaction flow , 2014 .

[10]  James L. Brown,et al.  Experimental Database with Baseline CFD Solutions: 2-D and Axisymmetric Hypersonic Shock-Wave/Turbulent-Boundary-Layer Interactions , 2013 .

[11]  Datta V. Gaitonde,et al.  Progress in shock wave/boundary layer interactions , 2013 .

[12]  N. Georgiadis,et al.  Status of turbulence modeling for hypersonic propulsion flowpaths , 2011 .

[13]  Peter A. Gnoffo,et al.  Uncertainty Assessment of Hypersonic Aerothermodynamics Prediction Capability , 2011 .

[14]  Krishnendu Sinha,et al.  Shock-unsteadiness model applied to oblique shock wave/turbulent boundary-layer interaction , 2008 .

[15]  Christopher J. Roy,et al.  Review and assessment of turbulence models for hypersonic flows , 2006 .

[16]  A. Panaras Calculation of flows characterized by extensive crossflow separation , 2004 .

[17]  Erich Schülein,et al.  Optical Skin Friction Measurements in Short-duration Facilities (Invited) , 2004 .

[18]  D. Knight,et al.  Advances in CFD prediction of shock wave turbulent boundary layer interactions , 2003 .

[19]  S. Deck,et al.  Development and application of Spalart–Allmaras one equation turbulence model to three-dimensional supersonic complex configurations , 2002 .

[20]  Frederic Thivet,et al.  Lessons Learned from RANS Simulations of Shock-Wave/Boundary-Layer Interactions , 2002 .

[21]  M. Y. Hussaini On Large-Eddy Simulation of Compressible Flows , 1998 .

[22]  A. Panaras,et al.  The effect of the structure of swept-shock-wave/turbulent-boundary-layer interactions on turbulence modelling , 1997, Journal of Fluid Mechanics.

[23]  J. Edwards,et al.  Comparison of eddy viscosity-transport turbulence models for three-dimensional, shock-separated flowfields , 1994 .

[24]  Farrukh S. Alvi,et al.  Physical Model of the Swept Shock Wave/Boundary-Layer Interaction Flowfield , 1992 .

[25]  P. Spalart A One-Equation Turbulence Model for Aerodynamic Flows , 1992 .

[26]  Krishnan Mahesh,et al.  Modeling the effect of shock unsteadiness in shock/ turbulent boundary-layer interactions , 2005 .

[27]  John L. Stollery,et al.  An experimental study of the interaction between a glancing shock wave and a turbulent boundary layer , 2005 .

[28]  I. Nompelis,et al.  Computational study of hypersonic double-cone experiments for code validation , 2004 .

[29]  Stephane Catris,et al.  Density corrections for turbulence models , 2000 .

[30]  Doyle,et al.  Shock Wave Boundary Layer Interactions in High Mach Number Flows A Critical Survey of Current Numerical Prediction Capabilities , 2000 .

[31]  G. Candler,et al.  Convergence improvement of two-equation turbulence model calculations , 1998 .

[32]  A. Panaras,et al.  Review of the physics of swept-shock/boundary layer interactions , 1996 .

[33]  Edney ANOMALOUS HEAT TRANSFER AND PRESSURE DISTRIBUTIONS ON BLUNT BODIES AT HYPERSONIC SPEEDS IN THE PRESENCE OF AN IMPINGING SHOCK. , 1968 .