Prefactored small-stencil compact schemes R Hixon Journal of Computational Physics 165 (2), 522-541, 2000 | 140 | 2000 |
Compact implicit MacCormack-type schemes with high accuracy R Hixon, E Turkel Journal of Computational Physics 158 (1), 51-70, 2000 | 130 | 2000 |
Evaluation of boundary conditions for computational aeroacoustics R Hixon, SH Shih, RR Mankabadi AIAA journal 33 (11), 2006-2012, 1995 | 121 | 1995 |
High-accuracy large-step explicit Runge–Kutta (HALE-RK) schemes for computational aeroacoustics V Allampalli, R Hixon, M Nallasamy, SD Sawyer Journal of Computational Physics 228 (10), 3837-3850, 2009 | 103 | 2009 |
Use of linearized Euler equations for supersonic jet noise prediction RR Mankbadi, R Hixon, SH Shih, LA Povinelli AIAA journal 36 (2), 140-147, 1998 | 102 | 1998 |
On increasing the accuracy of MacCormack schemes for aeroacoustic applications R Hixon, R Hixon 3rd AIAA/CEAS Aeroacoustics Conference, 1586, 1997 | 79 | 1997 |
A new class of compact schemes R Hixon 36th AIAA Aerospace Sciences Meeting and Exhibit, 367, 1998 | 61 | 1998 |
Evaluation of a high-accuracy MacCormack-type scheme using benchmark problems R Hixon Journal of Computational Acoustics 6 (03), 291-305, 1998 | 59 | 1998 |
Application of a nonlinear computational aeroacoustics code to the gust-airfoil problem R Hixon, V Golubev, RR Mankbadi, JR Scott, S Sawyer, M Nallasamy AIAA journal 44 (2), 323-328, 2006 | 58 | 2006 |
Evaluation of boundary conditions for the gust-cascade problem R Hixon, SH Shih, RR Mankbadi Journal of Propulsion and Power 16 (1), 72-78, 2000 | 42 | 2000 |
Toward low‐noise synthetic turbulent inflow conditions for aeroacoustic calculations A Sescu, R Hixon International Journal for Numerical Methods in Fluids 73 (12), 1001-1010, 2013 | 38 | 2013 |
Direct computation of jet noise produced by large-scale axisymmetric structures RR Mankbadi, SH Shih, R Hixon, LA Povinelli Journal of Propulsion and Power 16 (2), 207-215, 2000 | 36 | 2000 |
Zonal approach for prediction of jet noise SH Shih, DR Hixon, RR Mankbadi Journal of propulsion and power 13 (6), 745-752, 1997 | 36 | 1997 |
Parallelization strategy for an explicit computational aeroacoustics code R Hixon, M Nallasamy, S Sawyer 8th AIAA/CEAS Aeroacoustics Conference & Exhibit, 2583, 2002 | 35 | 2002 |
High-accuracy compact MacCormack-type schemes for computational aeroacoustics R Hixon, E Turkel 36th AIAA Aerospace Sciences Meeting and Exhibit, 365, 1998 | 31 | 1998 |
Radiation and wall boundary conditions for computational aeroacoustics: A review R Hixon International Journal of Computational Fluid Dynamics 18 (6), 523-531, 2004 | 29 | 2004 |
A computational aeroacoustic prediction of discrete-frequency rotor-stator interaction noise-a linear theory analysis S Sawyer, M Nallasamy, R Hixon, RW Dyson International Journal of Aeroacoustics 3 (1), 67-86, 2004 | 28 | 2004 |
Multidimensional optimization of finite difference schemes for computational aeroacoustics A Sescu, R Hixon, AA Afjeh Journal of Computational Physics 227 (9), 4563-4588, 2008 | 27 | 2008 |
Solution of unsteady Euler equations: Gust–cascade interaction tones M Nallasamy, R Hixon, S Sawyer Computers & fluids 36 (4), 724-741, 2007 | 24 | 2007 |
Space-time mapping analysis of airfoil nonlinear interaction with unsteady inviscid flow VV Golubev, RR Mankbadi, R Hixon AIAA journal 43 (10), 2147-2156, 2005 | 24 | 2005 |