Limitations in Turbomachinery CFD
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[1] L. Richardson. The Approximate Arithmetical Solution by Finite Differences of Physical Problems Involving Differential Equations, with an Application to the Stresses in a Masonry Dam , 1911 .
[2] Ronald Scott Bunker,et al. The Effects of Manufacturing Tolerances on Gas Turbine Cooling , 2009 .
[3] Li He,et al. An Euler Solution for Unsteady Flows Around Oscillating Blades , 1990 .
[4] L. He,et al. Method of Simulating Unsteady Turbomachinery Flows with Multiple Perturbations , 1992 .
[5] Simone Salvadori,et al. Simulation of Combustor/NGV Interaction Using Coupled RANS Solvers: Validation and Application to a Realistic Test Case , 2014 .
[6] Graham Pullan,et al. Secondary flows and loss caused by blade row interaction in a turbine stage , 2006 .
[7] Michael B. Giles,et al. Stator/rotor interaction in a transonic turbine , 1988 .
[8] P. Roache. Verification of Codes and Calculations , 1998 .
[9] Francesco Martelli,et al. Numerical Predictions of Film Cooled NGV Blades , 2003 .
[10] Jiang Luo,et al. Conjugate heat transfer analysis of a cooled turbine vane using the V2F turbulence model , 2007 .
[11] P. Roache. QUANTIFICATION OF UNCERTAINTY IN COMPUTATIONAL FLUID DYNAMICS , 1997 .
[12] Ismail Celik. Numerical uncertainty in fluid flow calculations: Needs for future research , 1993 .
[13] Francesco Montomoli,et al. Geometrical Uncertainty and Film Cooling: Fillet Radii , 2012 .
[14] Johannes Janicka,et al. A Compressible Pressure-based Solution Algorithm for Gas Turbine Combustion Chambers Using the PDF/FGM Model , 2013 .
[15] H. D. Joslyn,et al. Redistribution of an inlet temperature distortion in an axial flow turbine stage , 1989 .
[16] D. K. Walters,et al. A Three-Equation Eddy-Viscosity Model for Reynolds-Averaged Navier-Stokes Simulations of Transitional Flow , 2008 .
[17] K. Ghia,et al. Editorial Policy Statement on the Control of Numerical Accuracy , 1986 .
[18] Francesco Montomoli,et al. Geometrical uncertainty in turbomachinery: Tip gap and fillet radius , 2011 .
[19] R. Prim,et al. On the Multiplicity of Steady Gas Flows Having the Same Streamline Pattern. , 1947, Proceedings of the National Academy of Sciences of the United States of America.
[20] Thomas Povey,et al. Analysis on the Effect of a Nonuniform Inlet Profile on Heat Transfer and Fluid Flow in Turbine Stages , 2012 .
[21] HighWire Press. Philosophical Transactions of the Royal Society of London , 1781, The London Medical Journal.
[22] Kazunori Watanabe,et al. Assessment of URANS and DES for prediction of leading edge film cooling , 2012 .
[23] Guillermo Paniagua,et al. Energy Analysis of Pulsating Coolant Ejection , 2014 .
[24] Mauro Carnevale,et al. A Comparative Study of RANS, URANS and NLES Approaches for Flow Prediction in Pin Fin Array , 2013 .
[25] Guillermo Paniagua,et al. Aerothermal Impact of Stator-Rim Purge Flow and Rotor-Platform Film Cooling on a Transonic Turbine Stage , 2010 .
[26] F. Martelli,et al. Turbine blade boundary layer separation suppression via synthetic jet: An experimental and numerical study , 2012 .
[27] Roger L. Davis,et al. Unsteady analysis of hot streak migration in a turbine stage , 1990 .
[28] Simone Salvadori,et al. Conjugate Heat Transfer Analysis of a Film Cooled High-Pressure Turbine Vane Under Realistic Combustor Exit Flow Conditions , 2014 .
[29] Juan J. Alonso,et al. Integrated Simulations for Multi-Component Analysis of Gas Turbines:RANS Boundary Conditions , 2004 .
[30] Man Mohan Rai,et al. Multi-airfoil Navier-Stokes simulations of turbine rotor-stator interaction , 1988 .
[31] Roger W. Ainsworth,et al. Unsteady loss in a high pressure turbine stage: Interaction effects , 2005 .
[32] P. Roache. Perspective: A Method for Uniform Reporting of Grid Refinement Studies , 1994 .
[33] M. L. Celestina,et al. A model for closing the inviscid form of the average−passage equation system , 1986 .
[34] F. Lien,et al. Computations of transonic flow with the v2–f turbulence model , 2001 .
[35] Roger L. Davis,et al. UNSTEADY MULTISTAGE ANALYSIS USING A LOOSELY COUPLED BLADE ROW APPROACH , 1996 .
[36] L. Richardson,et al. The Deferred Approach to the Limit. Part I. Single Lattice. Part II. Interpenetrating Lattices , 1927 .
[37] Francesco Martelli,et al. Conjugate Heat Transfer Modelling in Film Cooled Blades , 2004 .
[38] Francesco Martelli,et al. Analysis of the shroud leakage flow and mainflow interactions in high-pressure turbines using an unsteady computational fluid dynamics approach , 2007 .
[39] G. Medic,et al. Integrated RANS/LES Computations of an Entire Gas Turbine Jet Engine , 2007 .
[40] J. L. Kerrebrock,et al. Intra-Stator Transport of Rotor Wakes and Its Effect on Compressor Performance , 1970 .
[41] Elena Collado Morata,et al. Impact of the unsteady aerothermal environment on the turbine blades temperature , 2012 .
[42] Michael B. Giles,et al. Calculation of Unsteady Wake/Rotor Interaction , 1987 .
[43] Francesco Montomoli,et al. Uncertainty Quantification: A Stochastic Method for Heat Transfer Prediction Using LES , 2013 .