Coupling of an Unsteady Aerodynamics Model with a Computational Fluid Dynamics Solver

Momentum source methods are an efficient means of representing airfoils in Navier–Stokes computational fluid dynamics (CFD) simulations. Momentum source terms are added to the Navier–Stokes equatio...

[1]  Wen Zhong Shen,et al.  The Actuator Surface Model: A New Navier-Stokes Based Model for Rotor Computations , 2009 .

[2]  Robert T Jones,et al.  Correction of the lifting-line theory for the effect of the chord , 1941 .

[3]  Christian Masson,et al.  Modeling of lifting-device aerodynamics using the actuator surface concept , 2009 .

[4]  Sheila E. Widnall,et al.  Helicopter Noise due to Blade‐Vortex Interaction , 1971 .

[5]  George N. Barakos,et al.  CFD analysis of complete helicopter configurations – lessons learnt from the GOAHEAD project , 2012 .

[6]  M. Scully,et al.  Computation of helicopter rotor wake geometry and its influence on rotor harmonic airloads , 1975 .

[7]  Nathan Hariharan,et al.  AIAA Standardized Hover Simulation: Hover Performance Prediction Status and Outstanding Issues , 2017 .

[8]  A. Gosman,et al.  Solution of the implicitly discretised reacting flow equations by operator-splitting , 1986 .

[9]  F. Porté-Agel,et al.  A Wind-Tunnel Investigation of Wind-Turbine Wakes: Boundary-Layer Turbulence Effects , 2009 .

[10]  Jens Nørkær Sørensen,et al.  Numerical Modeling of Wind Turbine Wakes , 2002 .

[11]  Gareth D. Padfield,et al.  Ship-Helicopter Operating Limits Prediction Using Piloted Flight Simulation and Time-Accurate Airwakes , 2012 .

[12]  J. P. V. Doormaal,et al.  ENHANCEMENTS OF THE SIMPLE METHOD FOR PREDICTING INCOMPRESSIBLE FLUID FLOWS , 1984 .

[13]  D. Telionis,et al.  PARALLEL BLADE–VORTEX INTERACTION , 1998 .

[14]  A. T. Conlisk,et al.  Modern helicopter rotor aerodynamics , 2001 .

[15]  F. Menter Two-equation eddy-viscosity turbulence models for engineering applications , 1994 .

[16]  Sven Schmitz,et al.  Guidelines for Volume Force Distributions Within Actuator Line Modeling of Wind Turbines on Large-Eddy Simulation-Type Grids , 2014 .

[17]  Sanjay R. Mathur,et al.  Three dimensional analysis of a rotor in forward flight , 1993 .

[18]  Johan Meyers,et al.  Optimal turbine spacing in fully developed wind farm boundary layers , 2012 .

[19]  George N. Barakos,et al.  A review of helicopter rotor blade tip shapes , 2013 .

[20]  R. Haimes,et al.  On the velocity gradient tensor and fluid feature extraction , 1999 .

[21]  Ismet Gursul,et al.  Effect of Steady Blowing on Wing Tip Flowfield , 2004 .

[22]  V. Venkatakrishnan,et al.  On the role and challenges of CFD in the aerospace industry , 2016, The Aeronautical Journal.

[23]  Forrester T. Johnson,et al.  THIRTY YEARS OF DEVELOPMENT AND APPLICATION OF CFD AT BOEING COMMERCIAL AIRPLANES, SEATTLE , 2005 .

[24]  Taewoo Kim,et al.  Improved actuator surface method for wind turbine application , 2015 .

[25]  B. V. Leer,et al.  Towards the ultimate conservative difference scheme. II. Monotonicity and conservation combined in a second-order scheme , 1974 .