Year |
Citation |
Score |
2020 |
Lyrintzis AS, Coderoni M. Overview of the Use of Large-Eddy Simulations in Jet Aeroacoustics Aiaa Journal. 58: 1620-1638. DOI: 10.2514/1.J058498 |
0.414 |
|
2019 |
Coderoni M, Lyrintzis AS, Blaisdell GA. Large-Eddy Simulations Analysis of Supersonic Heated Jets with Fluid Injection for Noise Reduction Aiaa Journal. 57: 3442-3455. DOI: 10.2514/1.J057674 |
0.501 |
|
2018 |
Coderoni M, Lyrintzis AS, Blaisdell GA. Noise reduction analysis of supersonic unheated jets with fluidic injection using large eddy simulations International Journal of Aeroacoustics. 17: 467-501. DOI: 10.1177/1475472X18778285 |
0.5 |
|
2017 |
Dhamankar NS, Blaisdell GA, Lyrintzis AS. Overview of Turbulent Inflow Boundary Conditions for Large-Eddy Simulations Aiaa Journal. 56: 1317-1334. DOI: 10.2514/1.J055528 |
0.41 |
|
2016 |
Mankbadi R, Lo S, Lyrintzis A, Golubev V, Dewan Y, Kurbatskii K. Hybrid LES-RANS simulations of a jet impinging on a flat plate International Journal of Aeroacoustics. 15: 535-553. DOI: 10.1177/1475472X16642355 |
0.511 |
|
2016 |
Dhamankar NS, Blaisdell GA, Lyrintzis AS. A simple extension of digital filter-based turbulent inflow to non-uniform structured grids Aerospace Science and Technology. 56: 29-33. DOI: 10.1016/J.Ast.2016.06.023 |
0.519 |
|
2016 |
Dhamankar NS, Blaisdell GA, Lyrintzis AS. Analysis of turbulent jet flow and associated noise with round and Chevron Nozzles using large Eddy simulation 22nd Aiaa/Ceas Aeroacoustics Conference, 2016. |
0.497 |
|
2015 |
Kube-McDowell MT, Blaisdell GA, Lyrintzis AS. Empirical source strength correlations for RANS-based acoustic analogy methods 53rd Aiaa Aerospace Sciences Meeting. DOI: 10.2514/6.2015-1005 |
0.823 |
|
2015 |
Aikens KM, Blaisdell GA, Lyrintzis AS. Analysis of converging-diverging beveled nozzle jets using large eddy simulation with a wall model 53rd Aiaa Aerospace Sciences Meeting. DOI: 10.2514/6.2015-0509 |
0.852 |
|
2015 |
Swift SH, Blaisdell GA, Lyrintzis AS. An efficient time-domain equivalent source method for acoustic scattering International Journal of Aeroacoustics. 14: 133-160. DOI: 10.1260/1475-472X.14.1-2.133 |
0.362 |
|
2015 |
Dhamankar NS, Blaisdell GA, Lyrintzis AS. Implementation of a sharp immersed boundary method in a 3-D Multi-block large eddy simulation tool for jet aeroacoustics 53rd Aiaa Aerospace Sciences Meeting. |
0.503 |
|
2014 |
Lyrintzis A, Golubev V, Kurbatski K, Osman E, Mankbadi R. Detached-Eddy simulations of rocket plume noise at lift-off Journal of the Acoustical Society of America. 136: 2168-2168. DOI: 10.1121/1.4899846 |
0.535 |
|
2014 |
Situ Y, Martha CS, Louis ME, Li Z, Sameh AH, Blaisdell GA, Lyrintzis AS. Petascale large eddy simulation of jet engine noise based on the truncated SPIKE algorithm Parallel Computing. 40: 496-511. DOI: 10.1016/j.parco.2014.07.002 |
0.832 |
|
2014 |
Aikens KM, Dhamankar NS, Martha CS, Situ Y, Blaisdell GA, Lyrintzis AS, Li Z. Equilibrium wall model for large eddy simulations of jets for aeroacoustics 52nd Aerospace Sciences Meeting. |
0.821 |
|
2014 |
Dhamankar NS, Martha CS, Situ Y, Aikens KM, Blaisdell GA, Lyrintzis AS, Li Z. Digital filter-based turbulent inflow generation for jet aeroacoustics on non-uniform structured grids 52nd Aerospace Sciences Meeting. |
0.857 |
|
2014 |
Dhamankar NS, Martha CS, Situ Y, Aikens KM, Blaisdell GA, Lyrintzis AS, Li Z. Digital filter-based turbulent inflow generation for jet aeroacoustics on non-uniform structured grids 52nd Aerospace Sciences Meeting. |
0.835 |
|
2014 |
Kurbatskii KA, Guenthoer BF, Golubev VV, Lyrintzis AS, Mankbadi RR, Osman E. Effect of inclination angle on mean flow and noise radiation from impinging rocket plume 20th Aiaa/Ceas Aeroacoustics Conference. |
0.434 |
|
2013 |
Martha CS, Blaisdell GA, Lyrintzis AS. Large eddy simulations of 2-D and 3-D spatially developing mixing layers Aerospace Science and Technology. 31: 59-72. DOI: 10.1063/1.3696302 |
0.803 |
|
2013 |
Martha CS, Blaisdell GA, Lyrintzis AS. Large eddy simulations of 2-D and 3-D spatially developing mixing layers Aerospace Science and Technology. 31: 59-72. DOI: 10.1016/J.Ast.2013.09.007 |
0.836 |
|
2013 |
Situ Y, Liu L, Martha CS, Louis ME, Li Z, Sameh AH, Blasidell GA, Lyrintzis AS. A communication-efficient linear system solver for large eddy simulation of jet engine noise Cluster Computing. 16: 157-170. DOI: 10.1007/S10586-011-0180-9 |
0.828 |
|
2013 |
Dewan Y, Golubev VV, Lyrintzis AS, Mankbadi RR, Kurbatskii KA, Osman E. Detached Eddy Simulations of supersonic jets impinging on flat plates 43rd Fluid Dynamics Conference. |
0.41 |
|
2012 |
Shurtz T, Blaisdell GA, Lyrintzis AS. Suitability of detached eddy simulation in overflow for predicting environments near supersonic jets 50th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. DOI: 10.2514/6.2012-888 |
0.401 |
|
2012 |
Martha CS, Situ Y, Louis ME, Blaisdell GA, Lyrintzis AS, Li Z. Development and application of an efficient, multiblock 3-D large eddy simulation tool for jet noise 50th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. DOI: 10.2514/6.2012-833 |
0.856 |
|
2012 |
Lillard RP, Oliver AB, Olsen ME, Blaisdell GA, Lyrintzis AS. The lagRST model: A turbulence model for non-equilibrium flows 50th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. DOI: 10.2514/6.2012-444 |
0.753 |
|
2012 |
Namgoong H, Crossley WA, Lyrintzis AS. Morphing airfoil design for minimum drag and actuation energy including aerodynamic work Journal of Aircraft. 49: 981-990. DOI: 10.2514/1.C031395 |
0.307 |
|
2012 |
Lo SC, Aikens KM, Blaisdell GA, Lyrintzis AS. Numerical investigation of 3-D supersonic jet flows using large-eddy simulation International Journal of Aeroacoustics. 11: 783-812. DOI: 10.1260/1475-472X.11.7-8.783 |
0.854 |
|
2011 |
Lyrintzis AS, Blaisdell GA. Jet noise predictions using large eddy simulations Recent Researches in Mechanics - Proc. of the 2nd Int. Conf. On Fluidsheat'11, Tam'11,Proc. of the 4th Wseas Int. Conf. Upt'11, Cuht'11. 196-200. |
0.469 |
|
2011 |
Thirumurthy D, Blaisdell GA, Lyrintzis AS, Sullivan JP. Preliminary design and computational analysis of an ejector nozzle with chevrons 49th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.372 |
|
2010 |
Lew PT, Mongeau L, Lyrintzis A. Noise prediction of a subsonic turbulent round jet using the lattice-Boltzmann method. The Journal of the Acoustical Society of America. 128: 1118-27. PMID 20815448 DOI: 10.1121/1.3458846 |
0.777 |
|
2010 |
Situ Y, Liu L, Martha CS, Louis ME, Li Z, Sameh AH, Blaisdell GA, Lyrintzis AS. Reducing communication overhead in large eddy simulation of jet engine noise Proceedings - Ieee International Conference On Cluster Computing, Iccc. 255-264. DOI: 10.1109/CLUSTER.2010.31 |
0.832 |
|
2010 |
Gross N, Blaisdell GA, Lyrintzis AS. Evaluation of turbulence model corrections for supersonic jets using the OVERFLOW code 40th Aiaa Fluid Dynamics Conference. |
0.316 |
|
2010 |
Thirumurthy D, Jones JT, Blaisdell GA, Lyrintzis AS, Sullivan JP. Experimental investigation and computation of a supersonic ejector nozzle with clamshells 40th Aiaa Fluid Dynamics Conference. |
0.445 |
|
2009 |
Lyrintzis A. Review of "Large-Eddy Simulation for Acoustics" Aiaa Journal. 47: 796-797. DOI: 10.2514/1.42646 |
0.342 |
|
2008 |
Kube-McDowell MT, Lyrintzis AS, Blaisdell GA. Parametric study of the generation of shocks in near-critical turbofan nozzles 14th Aiaa/Ceas Aeroacoustics Conference (29th Aiaa Aeroacoustics Conference). DOI: 10.2514/1.45691 |
0.8 |
|
2008 |
Pan FL, Uzun A, Lyrintzis AS. Surface integral methods in jet aeroacoustics: Refraction corrections Journal of Aircraft. 45: 381-387. DOI: 10.2514/1.23513 |
0.712 |
|
2008 |
Lo SC, Blaisdell GA, Lyrintzis AS. Numerical simulation of supersonic jet flows and their noise 14th Aiaa/Ceas Aeroacoustics Conference (29th Aiaa Aeroacoustics Conference). |
0.501 |
|
2008 |
Oliver AB, Lillard RP, Blaisdell GA, Lyrintzis AS. Effects of three-dimensionality in turbulent compression ramp shock-boundary layer interaction computations 46th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.79 |
|
2007 |
Lo SC, Blaisdell GA, Lyrintzis AS. High-order shock capturing schemes for turbulence calculations Collection of Technical Papers - 45th Aiaa Aerospace Sciences Meeting. 15: 10044-10061. DOI: 10.1002/Fld.2021 |
0.42 |
|
2007 |
Lo SC, Blaisdell GA, Lyrintzis AS. High-order shock capturing schemes for turbulence calculations Collection of Technical Papers - 45th Aiaa Aerospace Sciences Meeting. 15: 10044-10061. |
0.306 |
|
2007 |
Lew PT, Blaisdell GA, Lyrintzis AS. Investigation of noise sources in turbulent hot jets using large eddy simulation data Collection of Technical Papers - 45th Aiaa Aerospace Sciences Meeting. 1: 65-96. |
0.71 |
|
2007 |
Oliver AB, Lillard RP, Schwing AM, Blaisdell GA, Lyrintzis AS. Assessment of turbulent shock-boundary layer interaction computations using the OVERFLOW code Collection of Technical Papers - 45th Aiaa Aerospace Sciences Meeting. 2: 1182-1212. |
0.786 |
|
2006 |
Uzun A, Blaisdell GA, Lyrintzis AS. Impact of subgrid-scale models on jet turbulence and noise Aiaa Journal. 44: 1365-1368. DOI: 10.2514/1.9608 |
0.677 |
|
2006 |
Wright CW, Blaisdell GA, Lyrintzis AS. Investigating correlations between Reynolds-averaged flowfields and noise for forced mixed jets Journal of Aircraft. 43: 886-894. DOI: 10.2514/1.12555 |
0.591 |
|
2006 |
Garrison LA, Dalton WN, Lyrintzis AS, Blaisdell GA. Semi-Empirical Noise Models for Forced Mixer Jet Noise Predictions International Journal of Aeroacoustics. 5: 139-171. DOI: 10.1260/147547206777629862 |
0.838 |
|
2006 |
Lew P, Uzun A, Blaisdell GA, Lyrintzis AS. Development of a parallel 3-D les methodology for jet aeroacoustics via the schur complement Collection of Technical Papers - 44th Aiaa Aerospace Sciences Meeting. 13: 9561-9582. |
0.754 |
|
2006 |
Garrison LA, Lyrintzis AS, Blaisdell GA. RANS-based noise predictions of jets with internal forced mixers Collection of Technical Papers - 12th Aiaa/Ceas Aeroacoustics Conference. 4: 2553-2573. |
0.851 |
|
2006 |
Oliver AB, Lillard RP, Blaisdell GA, Lyrintzis AS. Validation of high-speed turbulent boundary layer and shock-boundary layer interaction computations with the OVERFLOW code Collection of Technical Papers - 44th Aiaa Aerospace Sciences Meeting. 14: 10677-10694. |
0.778 |
|
2005 |
Lew P, Blaisdell GA, Lyrintzis AS. Recent progress of hot jet aeroacoustics using 3-D large-eddy simulation Collection of Technical Papers - 11th Aiaa/Ceas Aeroacoustics Conference. 5: 3525-3548. |
0.747 |
|
2005 |
Garrison LA, Lyrintzis AS, Blaisdell GA, Dalton WN. Computational fluid dynamics analysis of jets with internal forced mixers Collection of Technical Papers - 11th Aiaa/Ceas Aeroacoustics Conference. 2: 1141-1160. |
0.791 |
|
2004 |
Uzun A, Lyrintzis AS, Blaisdell GA. Coupling of integral acoustics methods with LES for jet noise prediction International Journal of Aeroacoustics. 3: 297-346. DOI: 10.1260/1475472043499290 |
0.753 |
|
2004 |
Zhang X, Blaisdell GA, Lyrintzis AS. High-order compact schemes with filters on multi-block domains Journal of Scientific Computing. 21: 321-339. DOI: 10.1007/S10915-004-1320-7 |
0.382 |
|
2004 |
Uzun A, Blaisdell GA, Lyrintzis AS. Application of compact schemes to large eddy simulation of turbulent jets Journal of Scientific Computing. 21: 283-319. DOI: 10.1007/S10915-004-1319-0 |
0.742 |
|
2004 |
Uzun A, Lyrintzis AS, Blaisdell GA. Coupling of integral acoustics methods with LES for jet noise prediction Aiaa Paper. 4982-5001. |
0.716 |
|
2004 |
Pan FL, Uzun A, Lyrintzis AS. Refraction corrections for surface integral methods in jet aeroacoustics Collection of Technical Papers - 10th Aiaa/Ceas Aeroacoustics Conference. 1: 858-879. |
0.686 |
|
2004 |
Wright G, Blaisdell GA, Lyrintzis AS. Using RANS to predict the performance of mixers in reducing jet noise Aiaa Paper. 10245-10268. |
0.499 |
|
2004 |
Lew P, Uzun A, Blaisdell GA, Lyrintzis AS. Effects of inflow forcing on jet noise using large Eddy simulation Aiaa Paper. 65-73. |
0.774 |
|
2004 |
Garrison LA, Dalton WN, Lyrintzis AS, Blaisdell GA. On the development of semi-empirical noise models for the prediction of the noise from jets with forced mixers Collection of Technical Papers - 10th Aiaa/Ceas Aeroacoustics Conference. 2: 1142-1161. |
0.831 |
|
2003 |
Uzun A, Blaisdell GA, Lyrintzis AS. Sensitivity to the Smagorinsky Constant in Turbulent Jet Simulations Aiaa Journal. 41: 2077-2079. DOI: 10.2514/2.1900 |
0.615 |
|
2003 |
Lyrintzis AS. Surface integral methods in computational aeroacoustics—From the (CFD) near-field to the (Acoustic) far-field International Journal of Aeroacoustics. 2: 95-128. DOI: 10.1260/147547203322775498 |
0.352 |
|
2003 |
Ekici K, Lyrintzis AS. A parallel Newton-Krylov method for Navier-Stokes rotorcraft codes International Journal of Computational Fluid Dynamics. 17: 225-230. DOI: 10.1080/1061856031000123599 |
0.69 |
|
2003 |
Uzun A, Blaisdell GA, Lyrintzis AS. Sensitivity to the Smagorinsky Constant in Turbulent Jet Simulations Aiaa Journal. 41: 2077-2079. |
0.679 |
|
2003 |
Uzun A, Blaisdell GA, Lyrintzis AS. 3-D Large Eddy Simulation for jet aeroacoustics 9th Aiaa/Ceas Aeroacoustics Conference and Exhibit. |
0.716 |
|
2003 |
Wright C, Blaisdell GA, Lyrintzis AS. The effects of various mixer shapes on jet noise 9th Aiaa/Ceas Aeroacoustics Conference and Exhibit. |
0.453 |
|
2003 |
Garrison LA, Dalton WN, Lyrintzis AS, Blaisdell GA. An investigation of the extension of the foursource method for predicting the noise from jets with internal forced mixers 9th Aiaa/Ceas Aeroacoustics Conference and Exhibit. |
0.831 |
|
2002 |
Kim H, Williams MH, Lyrintzis AS. Improved method for rotor wake capturing Journal of Aircraft. 39: 794-803. DOI: 10.2514/2.3025 |
0.412 |
|
2002 |
Ekici K, Lyrintzis AS. Parallelization of rotorcraft aerodynamics Navier-Stokes codes Aiaa Journal. 40: 887-896. DOI: 10.2514/2.1725 |
0.659 |
|
2002 |
Uzun A, Blaisdell GA, Lyrintzis AS. Recent progress towards a large eddy simulation code for jet aeroacoustics 8th Aiaa/Ceas Aeroacoustics Conference and Exhibit. |
0.682 |
|
2001 |
Lyrintzis AS, Uzun A. Integral techniques for jet aeroacoustics calculations 7th Aiaa/Ceas Aeroacoustics Conference and Exhibit. |
0.672 |
|
2001 |
Ekici K, Lyrintzis AS. Parallel newton-krylov methods for rot or craft aerodynamics 15th Aiaa Computational Fluid Dynamics Conference. |
0.664 |
|
2001 |
Kim H, Williams MH, Lyrintzis AS. An improved method for rotor wake capturing 15th Aiaa Computational Fluid Dynamics Conference. |
0.305 |
|
2001 |
Uzun A, Koutsavdis EK, Blaisdell GA, Lyrintzis AS. Direct numerical simulation of 3-D jets using compact schemes and spatial filtering 15th Aiaa Computational Fluid Dynamics Conference. |
0.843 |
|
2000 |
Caradonna F, Kitaplioglu C, McCluer M, Baeder J, Leishman JG, Berezin C, Visintainer J, Bridgeman J, Burley C, Epstein R, Lyrintzis A, Koutsavdis E, Rahier G, Delrieux Y, Rule J, et al. Methods for the Prediction of Blade-Vortex Interaction Noise Journal of the American Helicopter Society. 45: 303-317. DOI: 10.4050/Jahs.45.303 |
0.817 |
|
2000 |
Jones BR, Crossley WA, Lyrintzis AS. Aerodynamic and aeroacoustic optimization of rotorcraft airfoils via a parallel genetic algorithm Journal of Aircraft. 37: 1088-1096. DOI: 10.2514/2.2717 |
0.379 |
|
2000 |
Koutsavdis EK, Blaisdell GA, Lyrintzis AS. Compact Schemes with Spatial Filtering in Computational Aeroacoustics Aiaa Journal. 38: 713-715. DOI: 10.2514/2.1016 |
0.329 |
|
2000 |
Ekici K, Lyrintzis AS. Parallel computing techniques for rotorcraft aerodynamics Fluids 2000 Conference and Exhibit. |
0.644 |
|
2000 |
Koutsavdis EK, Blaisdell GA, Lyrintzis AS. Compact schemes with spatial filtering in computational aeroacoustics Aiaa Journal. 38: 713-715. |
0.77 |
|
2000 |
Lyrintzis AS, Jameson JR, Koutsavdis EK. Study of rotorcraft blade-tip shape high-speed impulsive noise characteristics Journal of the American Helicopter Society. 45: 54-57. |
0.82 |
|
1999 |
Wissink AM, Lyrintzis AS, Chronopoulos AT. Parallel Newton-Krylov method for rotary-wing flowfield calculations Aiaa Journal. 37: 1213-1221. DOI: 10.2514/2.615 |
0.411 |
|
1999 |
Koutsavdis EK, Blaisdell GA, Lyrintzis AS. A numerical investigation of two-dimensional jets using spatial filtering 5th Aiaa/Ceas Aeroacoustics Conference and Exhibit. |
0.803 |
|
1999 |
Koutsavdis EK, Blaisdell GA, Lyrintzis AS. On the use of compact schemes with spatialfiltering in Computational Aeroacoustics 37th Aerospace Sciences Meeting and Exhibit. |
0.777 |
|
1998 |
Lyrintzis AS, Koutsavdis EK, Berezin CR, Visintainer JA, Pollack MJ. An evaluation of a rotating Kirchhoff acoustic methodology Journal of the American Helicopter Society. 43: 57-65. DOI: 10.4050/Jahs.43.57 |
0.829 |
|
1998 |
Liu G, Lyrintzis AS, Michalopoulos PG. Improved high-order model for freeway traffic flow Transportation Research Record. 37-46. DOI: 10.3141/1644-05 |
0.371 |
|
1998 |
Pilon AR, Lyrintzis AS. Development of an improved Kirchhoff method for jet aeroacoustics Aiaa Journal. 36: 783-790. DOI: 10.2514/2.437 |
0.376 |
|
1998 |
Pilon AR, Lyrintzis AS. Mean flow refraction corrections for the Kirchhoff method Journal of Aircraft. 35: 661-664. DOI: 10.2514/2.2355 |
0.322 |
|
1998 |
Lyrintzis AS. Some recent advances in the use of kirchhoff's method in computational aeroacoustics American Society of Mechanical Engineers, Noise Control and Acoustics Division (Publication) Nca. 25: 453-467. |
0.378 |
|
1998 |
Spyropoulos JT, Douglas J, Lyrintzis AS. A new-scheme for the incompressible navier-stokes equations employing alternating-direction operator splitting and domain decomposition 36th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.304 |
|
1997 |
Lyrintzis AS, Koutsavdis EK, Strawn RC. Technical note: A comparison of computational aeroacoustic prediction methods Journal of the American Helicopter Society. 42: 54-57. DOI: 10.4050/Jahs.42.54 |
0.841 |
|
1997 |
Pilon AR, Lyrintzis AS. Refraction corrections for the Kirchhoff method 3rd Aiaa/Ceas Aeroacoustics Conference. 1-7. DOI: 10.2514/6.1997-1654 |
0.415 |
|
1997 |
Brentner KS, Lyrintzis AS, Koutsavdis EK. Comparison of computational aeroacoustic prediction methods for transonic rotor noise Journal of Aircraft. 34: 531-538. DOI: 10.2514/2.2205 |
0.82 |
|
1997 |
Liu G, Lyrintzis AS, Michalopoulos PG. Numerical simulation of freeway traffic flow Journal of Transportation Engineering. 123: 503-513. DOI: 10.1061/(Asce)0733-947X(1997)123:6(503) |
0.416 |
|
1997 |
Koutsavdis EK, Lyrintzis AS. An investigation of kirchhoff’s methodologies for computational aeroacoustics 35th Aerospace Sciences Meeting and Exhibit. |
0.774 |
|
1997 |
Wissink AM, Lyrintzis AS, Chronopoulos AT. A parallel Newton-Krylov method for rotorcraft flowfield calculations 13th Computational Fluid Dynamics Conference. 1060-1070. |
0.323 |
|
1997 |
Scott JN, Pilon AR, Lyrintzis AS, Rozmajzl TJ. A numerical investigation of noise from a rectangular jet 35th Aerospace Sciences Meeting and Exhibit. |
0.539 |
|
1996 |
Lyrintzis AS, Xue Y. Towards a versatile Kirchhoff code for aeroacoustic predictions 2nd Aiaa/Ceas Aeroacoustics Conference. DOI: 10.2514/6.1996-1710 |
0.338 |
|
1996 |
Pilon AR, Lyrintzis AS. An improved Kirchhoff method for jet aeroacoustics 2nd Aiaa/Ceas Aeroacoustics Conference. DOI: 10.2514/6.1996-1709 |
0.366 |
|
1996 |
Lyrintzis AS, Koutsavdis EK. Rotorcraft impulsive noise prediction using a rotating Kirchhoff formulation Journal of Aircraft. 33: 1054-1061. DOI: 10.2514/3.47057 |
0.84 |
|
1996 |
Pilon AR, Lyrintzis AS. Data-parallel total variation diminishing method for sonic boom calculations Journal of Aircraft. 33: 87-92. DOI: 10.2514/3.46907 |
0.424 |
|
1996 |
Wissink AM, Lyrintzis AS, Strawn RC. Parallelization of a three-dimensional flow solver for Euler rotorcraft aerodynamics predictions Aiaa Journal. 34: 2276-2283. DOI: 10.2514/3.13391 |
0.395 |
|
1996 |
Lyrintzis AS, Mankbadi RR. Prediction of the far-field jet noise using Kirchhoff's formulation Aiaa Journal. 34: 413-416. DOI: 10.2514/3.13079 |
0.455 |
|
1996 |
Strawn RC, Biswas R, Lyrintzis AS. Helicopter noise predictions using Kirchhoff methods Journal of Computational Acoustics. 4: 321-339. DOI: 10.1142/S0218396X96000106 |
0.553 |
|
1996 |
Liu G, Lyrintzis AS, Michalopoulos PG. Modelling of freeway merging and diverging flow dynamics Applied Mathematical Modelling. 20: 459-469. DOI: 10.1016/0307-904X(95)00165-G |
0.401 |
|
1996 |
Wissink AM, Lyrintzis AS, Chronopoulos AT. Efficient iterative methods applied to the solution of transonic flows Journal of Computational Physics. 123: 379-393. DOI: 10.1006/Jcph.1996.0031 |
0.359 |
|
1996 |
Wissink AM, Lyrintzis AS, Strawn RC, Oliker L, Biswas R. Efficient helicopter aerodynamic and aeroacoustic predictions on parallel computers 34th Aerospace Sciences Meeting and Exhibit. |
0.313 |
|
1995 |
Pilon AR, Lyrintzis AS. A data parallel TVD method for sonic boom calculations 33rd Aerospace Sciences Meeting and Exhibit. |
0.33 |
|
1995 |
Lyrintzis AS, Mankbadi RR. On the prediction of the far-field jet noise using Kirchhoff’s formulation 33rd Aerospace Sciences Meeting and Exhibit. |
0.357 |
|
1994 |
Olejniczak J, Lyrintzis AS. Design of optimized airfoils in subcritical flow Journal of Aircraft. 31: 680-687. DOI: 10.2514/3.46548 |
0.424 |
|
1994 |
Xue Y, Lyrintzis AS. Rotating Kirchhoff method for three-dimensional transonic blade-vortex interaction hover noise Aiaa Journal. 32: 1350-1359. DOI: 10.2514/3.12202 |
0.568 |
|
1994 |
Lyrintzis AS. Review: The use of Kirchhoff's method in computational aeroacoustics Journal of Fluids Engineering, Transactions of the Asme. 116: 665-676. DOI: 10.1115/1.2911834 |
0.384 |
|
1994 |
Lyrintzis AS, Lee J, Xue Y. Mechanisms and directivity of unsteady transonic flow noise Journal of Fluids Engineering, Transactions of the Asme. 116: 649-652. DOI: 10.1115/1.2910327 |
0.495 |
|
1994 |
Lyrintzis AS, Yi P, Michalopoulos PG, Beskos DE. Advanced continuum traffic flow models for congested freeways Journal of Transportation Engineering. 120: 461-477. DOI: 10.1061/(Asce)0733-947X(1994)120:3(461) |
0.357 |
|
1993 |
Xue Y, Lyrintzis AS. Transonic blade-vortex interactions - Noise reduction Journal of Aircraft. 30: 408-411. DOI: 10.2514/3.56888 |
0.521 |
|
1993 |
Chronopoulos A, Lyrintzis A, Michalopoulos P, Rhee C, Yi P. Traffic flow simulation through high order traffic modelling Mathematical and Computer Modelling. 17: 11-22. DOI: 10.1016/0895-7177(93)90150-W |
0.41 |
|
1993 |
Michalopoulos PG, Yi P, Lyrintzis AS. Continuum modelling of traffic dynamics for congested freeways Transportation Research Part B. 27: 315-332. DOI: 10.1016/0191-2615(93)90041-8 |
0.365 |
|
1993 |
Xue Y, Lyrintzis AS. Transonic blade-vortex interactions: noise reduction Journal of Aircraft. 30: 408-411. |
0.442 |
|
1992 |
Lyrintzis AS, Xue Y. Acoustics of transonic flow around an oscillating flap Journal of Fluids Engineering, Transactions of the Asme. 114: 240-245. DOI: 10.1115/1.2910021 |
0.506 |
|
1991 |
Lyrintzis AS, Xue Y. Study of the noise mechanisms of transonic blade-vortex interactions Aiaa Journal. 29: 1562-1572. DOI: 10.2514/3.10776 |
0.555 |
|
1990 |
Lyrintzis AS, Xue Y. Acoustics of unsteady transonic flow American Society of Mechanical Engineers, Fluids Engineering Division (Publication) Fed. 92: 187-199. |
0.427 |
|
1990 |
Lyrintzis AS, Xue Y. Noise mechanisms of Transonic Blade-Vortex Interactions Annual Forum Proceedings - American Helicopter Society. 3. |
0.448 |
|
1989 |
Lyrintzis AS, George AR. Far field noise of transonic blade-vortex interactions Journal of the American Helicopter Society. 34: 30-39. DOI: 10.4050/Jahs.34.30 |
0.81 |
|
1989 |
Lyrintzis AS, George AR. Use of the kirchhoff method in acoustics Aiaa Journal. 27: 1451-1453. DOI: 10.2514/3.10285 |
0.441 |
|
1989 |
Lyrintzis AS, George AR. Technical note: study of transonic blade-vortex interaction noise Noise Control Engineering Journal. 32: 105-109. |
0.416 |
|
1988 |
George AR, Lyrintzis AS. Acoustics of transonic blade-vortex interactions Aiaa Journal. 26: 769-776. DOI: 10.2514/3.9968 |
0.467 |
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