High Order Accurate Finite-Difference Methods: as seen in OVERFLOW

Conventional nite-di erence methods are the main workhorse of NASA's OVERFLOW code. Recent enhancements in the development, implementation and analysis of simple high-order accurate nite-di erence techniques within OVERFLOW are documented here. Results are presented for simple vortex propagation to demonstrate the salient features of the methods, and more complex three-dimensional rotorcraft ows are used to validate their usefulness in real applications.

[1]  William M. Chan,et al.  Overset grid technology development at NASA Ames Research Center , 2009 .

[2]  J. Benek,et al.  A 3-D Chimera Grid Embedding Technique , 1985 .

[3]  Neal Chaderjian,et al.  High Resolution Navier-Stokes Simulation of Rotor Wakes , 2011 .

[4]  Jeffrey L. Johnson,et al.  Tilt Rotor Aeroacoustic Model Project , 1999 .

[5]  R. F. Warming,et al.  An implicit finite-difference algorithm for hyperbolic systems in conservation-law form. [application to Eulerian gasdynamic equations , 1976 .

[6]  Thomas H. Pulliam,et al.  Large Scale Aerodynamic Calculation on Pleiades , 2009 .

[7]  Robert L. Meakin,et al.  Object X-Rays for Cutting Holes in Composite Overset Structured Grids , 2001 .

[8]  T. Pulliam,et al.  A diagonal form of an implicit approximate-factorization algorithm , 1981 .

[9]  Terry L. Holst,et al.  Overset Solution Adaptive Grid Approach Applied to Hovering Rotorcraft Flows , 2009 .

[10]  Robert L. Meakin,et al.  Automatic Off-Body Grid Generation for Domains of Arbitrary Size , 2001 .

[11]  Neal M. Chaderjian,et al.  High-Order Accurate CFD/CSD Simulation of the UH-60 Rotor in Forward Flight , 2011 .

[12]  Gloria K. Yamauchi,et al.  Airloads Measurements from a 1/4-Scale Tiltrotor Wind Tunnel Test , 1999 .

[13]  P. Spalart,et al.  A New Version of Detached-eddy Simulation, Resistant to Ambiguous Grid Densities , 2006 .

[14]  P. Spalart Comments on the feasibility of LES for wings, and on a hybrid RANS/LES approach , 1997 .

[15]  Antony Jameson,et al.  Combined Feature-Driven Richardson-Based Adaptive Mesh Refinement for Unsteady Vortical Flows , 2012 .

[16]  Pieter G. Buning,et al.  Evaluation of Two High Order WENO Schemes , 2007 .

[17]  Thomas H. Pulliam,et al.  Artificial Dissipation Models for the Euler Equations , 1985 .

[18]  Robert H. Nichols,et al.  Solver and Turbulence Model Upgrades to OVERFLOW 2 for Unsteady and High-Speed Applications , 2006 .

[19]  J. Steger,et al.  Implicit Finite-Difference Simulations of Three-Dimensional Compressible Flow , 1980 .

[20]  Roger C. Strawn,et al.  CFD Simulations of Tiltrotor Configurations in Hover , 2005 .

[21]  Stuart E. Rogers,et al.  Pegasus 5: An Automated Pre-Processor for Overset-Grid Cfd , 2013 .

[22]  J. Steger,et al.  Flux vector splitting of the inviscid gasdynamic equations with application to finite-difference methods , 1981 .

[23]  T. Pulliam Efficient solution methods for the Navier-Stokes equations , 1986 .

[24]  P. Buning,et al.  Numerical simulation of the integrated space shuttle vehicle in ascent , 1988 .