Anastasios S. Lyrintzis - Publications

Affiliations: 
1994- Aeronautics and Astronautics Purdue University, West Lafayette, IN, United States 
Area:
Aerospace Engineering, Acoustics Physics
Website:
https://engineering.purdue.edu/AAE/people/ptProfile?resource_id=1345

122 high-probability publications. We are testing a new system for linking publications to authors. You can help! If you notice any inaccuracies, please sign in and mark papers as correct or incorrect matches. If you identify any major omissions or other inaccuracies in the publication list, please let us know.

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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