| Year |
Citation |
Score |
| 2019 |
Esfahani A, Webb N, Samimy M. Flow Separation Control over a Thin Post-Stall Airfoil: Effects of Excitation Frequency Aiaa Journal. 57: 1826-1838. DOI: 10.2514/1.J057796 |
0.67 |
|
| 2019 |
Samimy M, Webb N, Esfahani A. Reinventing the wheel: excitation of flow instabilities for active flow control using plasma actuators Journal of Physics D: Applied Physics. 52: 354002. DOI: 10.1088/1361-6463/Ab272D |
0.663 |
|
| 2018 |
Samimy M, Webb N, Crawley M. Excitation of Free Shear-Layer Instabilities for High-Speed Flow Control Aiaa Journal. 56: 1770-1791. DOI: 10.2514/1.J056610 |
0.662 |
|
| 2018 |
Singhal A, Castañeda D, Webb N, Samimy M. Control of Dynamic Stall over a NACA 0015 Airfoil Using Plasma Actuators Aiaa Journal. 56: 78-89. DOI: 10.2514/1.J056071 |
0.599 |
|
| 2018 |
Crawley M, Gefen L, Kuo C, Samimy M, Camussi R. Vortex dynamics and sound emission in excited high-speed jets Journal of Fluid Mechanics. 839: 313-347. DOI: 10.1017/Jfm.2017.906 |
0.399 |
|
| 2018 |
Esfahani A, Webb N, Samimy M. Stall cell formation over a post-stall airfoil: effects of active perturbations using plasma actuators Experiments in Fluids. 59. DOI: 10.1007/S00348-018-2588-Y |
0.598 |
|
| 2017 |
Kuo C, Cluts J, Samimy M. Effects of excitation around jet preferred mode Strouhal number in high-speed jets Experiments in Fluids. 58: 35. DOI: 10.1007/S00348-017-2329-7 |
0.529 |
|
| 2016 |
Clifford C, Singhal A, Samimy M. Flow control over an airfoil in fully reversed condition using plasma actuators Aiaa Journal. 54: 141-149. DOI: 10.2514/1.J054157 |
0.477 |
|
| 2016 |
Crawley M, Kuo CW, Samimy M. Identification of the acoustic response in the irrotational near-field of an excited subsonic jet International Journal of Aeroacoustics. 15: 496-514. DOI: 10.1177/1475472X16642137 |
0.424 |
|
| 2016 |
Crawley M, Kuo CW, Samimy M. Vortex dynamics and sound emission in an excited high-speed jet 22nd Aiaa/Ceas Aeroacoustics Conference, 2016. |
0.444 |
|
| 2016 |
Cluts J, Kuo CW, Samimy M. Effects of excitation frequency and azimuthal mode on the flow, pressure, and acoustic fields of supersonic jets 22nd Aiaa/Ceas Aeroacoustics Conference, 2016. |
0.379 |
|
| 2015 |
Clifford C, Samimy M. Flow control on an airfoil in fully-reversed condition with actuation on both leading and trailing edges 53rd Aiaa Aerospace Sciences Meeting. DOI: 10.2514/6.2015-1266 |
0.364 |
|
| 2015 |
Crawley M, Speth RL, Gaitonde DV, Samimy M. A study of the noise source mechanisms in an excited mach 0.9 jet-complementary experimental and computational analysis 53rd Aiaa Aerospace Sciences Meeting. DOI: 10.2514/6.2015-0736 |
0.676 |
|
| 2015 |
Kim JH, Kim S, Samimy M. LES simulation of forced high-speed jet 53rd Aiaa Aerospace Sciences Meeting. DOI: 10.2514/6.2015-0300 |
0.365 |
|
| 2015 |
Cluts J, Kuo CW, Samimy M. Exploring physics and control of twin supersonic circular jets 53rd Aiaa Aerospace Sciences Meeting. DOI: 10.2514/1.J054977 |
0.537 |
|
| 2015 |
Crawley M, Sinha A, Samimy M. Near-Field and Acoustic Far-Field Response of a High-Speed Jet to Excitation Aiaa Journal. 53: 1894-1909. DOI: 10.2514/1.J053581 |
0.495 |
|
| 2015 |
Kuo CW, Crawley M, Samimy M. Near-field pressure waveform analysis of an excited Mach 0.9 jet 21st Aiaa/Ceas Aeroacoustics Conference. |
0.313 |
|
| 2015 |
Cluts J, Kuo CW, Samimy M. An investigation of twin supersonic Jets’ near-field 21st Aiaa/Ceas Aeroacoustics Conference. |
0.404 |
|
| 2013 |
Yugulis K, Gregory JW, Samimy M. Control of high subsonic cavity flow using plasma actuators 51st Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 2013. DOI: 10.2514/1.J052668 |
0.441 |
|
| 2013 |
Kearney-Fischer M, Sinha A, Samimy M. Intermittent nature of subsonic jet noise Aiaa Journal. 51: 1142-1155. DOI: 10.2514/1.J051930 |
0.801 |
|
| 2013 |
Sinha A, Serrani A, Samimy M. Reduced-order modeling of high-speed jets controlled by arc filament plasma actuators Experiments in Fluids. 54. DOI: 10.1007/S00348-012-1428-8 |
0.506 |
|
| 2013 |
Crawley M, Alkandry H, Sinha A, Samimy M. Correlation of irrotational near-field pressure and far-field acoustic in forced high-speed jets 19th Aiaa/Ceas Aeroacoustics Conference. 182. |
0.378 |
|
| 2012 |
Little J, Takashima K, Nishihara M, Adamovich I, Samimy M. Separation control with nanosecond-pulse-driven dielectric barrier discharge plasma actuators Aiaa Journal. 50: 350-365. DOI: 10.2514/1.J051114 |
0.443 |
|
| 2012 |
Samimy M, Kearney-Fischer M, Kim JH, Sinha A. High-speed and high-reynolds-number jet control using localized arc filament plasma actuators Journal of Propulsion and Power. 28: 269-280. DOI: 10.2514/1.B34272 |
0.831 |
|
| 2012 |
Kearney-Fischer M, Sinha A, Samimy M. Time-domain analysis of excited subsonic jet noise 18th Aiaa/Ceas Aeroacoustics Conference (33rd Aiaa Aeroacoustics Conference). DOI: 10.1260/1475-472X.12.4.387 |
0.799 |
|
| 2012 |
Sinha A, Alkandry H, Kearney-Fischer M, Samimy M. The impulse response of a high-speed jet forced with localized arc filament plasma actuators 18th Aiaa/Ceas Aeroacoustics Conference (33rd Aiaa Aeroacoustics Conference). DOI: 10.1063/1.4772191 |
0.804 |
|
| 2012 |
Sinha A, Alkandry H, Kearney-Fischer M, Samimy M. The impulse response of a high-speed jet forced with localized arc filament plasma actuators 18th Aiaa/Ceas Aeroacoustics Conference (33rd Aiaa Aeroacoustics Conference). DOI: 10.1063/1.4772191 |
0.793 |
|
| 2012 |
Webb N, Clifford C, Samimy M. Control of oblique shock wave-boundary layer interactions using plasma actuators 6th Aiaa Flow Control Conference 2012. DOI: 10.1007/S00348-013-1545-Z |
0.649 |
|
| 2012 |
Crawley M, Kearney-Fischer M, Samimy M. Control of a supersonic rectangular jet using plasma actuators 18th Aiaa/Ceas Aeroacoustics Conference (33rd Aiaa Aeroacoustics Conference). |
0.787 |
|
| 2012 |
Kearney-Fischer M, Sinha A, Samimy M. Time-domain analysis of subsonic jet noise 50th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.781 |
|
| 2012 |
Adamovich IV, Little J, Nishihara M, Takashima K, Samimy M. Nanosecond pulse surface discharges for high-speed flow control 6th Aiaa Flow Control Conference 2012. |
0.363 |
|
| 2011 |
Sinha A, Serrani A, Samimy M. Development of empirical estimators for feedback control of high-speed axisymmetric jets Aiaa Journal. 49: 1971-1987. DOI: 10.2514/1.J050966 |
0.452 |
|
| 2011 |
Rethmel C, Little J, Takashima K, Sinha A, Adamovich I, Samimy M. Flow Separation Control Using Nanosecond Pulse Driven DBD Plasma Actuators International Journal of Flow Control. 3: 213-232. DOI: 10.1260/1756-8250.3.4.213 |
0.514 |
|
| 2011 |
Kearney-Fischer M, Kim JH, Samimy M. Noise control of a high Reynolds number high speed heated jet using plasma actuators International Journal of Aeroacoustics. 10: 635-658. DOI: 10.1260/1475-472X.10.5-6.635 |
0.822 |
|
| 2011 |
Kim JH, Kearney-Fischer M, Samimy M, Gogineni S. Far-field noise control in supersonic jets from conical and contoured nozzles Journal of Engineering For Gas Turbines and Power. 133. DOI: 10.1115/1.4002811 |
0.82 |
|
| 2011 |
Gaitonde DV, Samimy M. Coherent structures in plasma-actuator controlled supersonic jets: Axisymmetric and mixed azimuthal modes Physics of Fluids. 23. DOI: 10.1063/1.3627215 |
0.659 |
|
| 2011 |
Kearney-Fischer M, Kim JH, Samimy M. A study of Mach wave radiation using active control Journal of Fluid Mechanics. 681: 261-292. DOI: 10.1017/Jfm.2011.196 |
0.77 |
|
| 2011 |
Hahn C, Kearney-Fischer M, Samimy M. On factors influencing arc filament plasma actuator performance in control of high speed jets Experiments in Fluids. 51: 1591-1603. DOI: 10.1007/S00348-011-1172-5 |
0.807 |
|
| 2011 |
Hahn C, Kearney-Fischer M, Samimy M. Effects of ring groove and duty cycle on plasma actuator performance in high speed jets 49th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.794 |
|
| 2011 |
Kearney-Fischer M, Kim JH, Samimy M. Study of mach wave radiation in an axisymmetric jet using active control 17th Aiaa/Ceas Aeroacoustics Conference 2011 (32nd Aiaa Aeroacoustics Conference). |
0.759 |
|
| 2011 |
Sinha A, Serrani A, Samimy M. Incorporating actuation effects in reduced-order models for feedback control of axisymmetric jets 17th Aiaa/Ceas Aeroacoustics Conference 2011 (32nd Aiaa Aeroacoustics Conference). |
0.365 |
|
| 2011 |
Gaitonde DV, Samimy M, Speth R. ILES of plasma-controlled jets-coherent features and near-field pressure response 40th International Congress and Exposition On Noise Control Engineering 2011, Inter-Noise 2011. 1: 271-278. |
0.624 |
|
| 2010 |
Little J, Samimy M. High-lift airfoil separation with dielectric barrier discharge plasma actuation Aiaa Journal. 48: 2884-2898. DOI: 10.2514/1.J050452 |
0.453 |
|
| 2010 |
Sinha A, Serrani A, Samimy M. Initial development of reduced-order models for feedback control of axisymmetric jets International Journal of Flow Control. 2: 39-60. DOI: 10.1260/1756-8250.2.1.39 |
0.436 |
|
| 2010 |
Samimy M, Kim JH, Kearney-Fischer M, Sinha A. Acoustic and flow fields of an excited high Reynolds number axisymmetric supersonic jet Journal of Fluid Mechanics. 656: 507-529. DOI: 10.1017/S0022112010001357 |
0.82 |
|
| 2010 |
Kim J, Nishihara M, Adamovich IV, Samimy M, Gorbatov SV, Pliavaka FV. Development of localized arc filament RF plasma actuators for high-speed and high Reynolds number flow control Experiments in Fluids. 49: 497-511. DOI: 10.1007/S00348-010-0819-Y |
0.389 |
|
| 2010 |
Little J, Nishihara M, Adamovich I, Samimy M. High-lift airfoil trailing edge separation control using a single dielectric barrier discharge plasma actuator Experiments in Fluids. 48: 521-537. DOI: 10.1007/S00348-009-0755-X |
0.472 |
|
| 2010 |
Gaitonde DV, Samimy M. Effect of plasma-based azimuthal mode excitation on supersonic jet flow 5th Flow Control Conference. |
0.62 |
|
| 2010 |
Kearney-Fischer M, Samimy M. Noise control of a high Reynolds number Mach 1.3 heated jet using plasma actuators 48th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.824 |
|
| 2010 |
Kearney-Fischer M, Kim JH, Samimy M. Flow control of a high Reynolds number Mach 1.3 heated jet using plasma actuators 5th Flow Control Conference. |
0.799 |
|
| 2010 |
Sinha A, Serrani A, Samimy M. Development of reduced-order models for feedback control of axisymmetric jets 48th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.452 |
|
| 2010 |
Little J, Takashima K, Nishihara M, Adamovich I, Samimy M. High lift airfoil leading edge separation control with nanosecond pulse driven DBD plasma actuators 5th Flow Control Conference. |
0.364 |
|
| 2009 |
Sinha A, Kim K, Kim JH, Serrani A, Samimy M. Extremizing feedback control of a high-speed and high Reynolds number jet 47th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. DOI: 10.2514/1.44012 |
0.554 |
|
| 2009 |
Kim JH, Kastner J, Samimy M. Active control of a high reynolds number Mach 0.9 axisymmetric Jet Aiaa Journal. 47: 116-128. DOI: 10.2514/1.36801 |
0.522 |
|
| 2009 |
Kastner J, Kim J, Samimy M. A Study of the Correlation of Large-Scale Structure Dynamics and Far-Field Radiated Noise in an Excited Mach 0.9 Jet International Journal of Aeroacoustics. 8: 231-259. DOI: 10.1260/147547208786940008 |
0.573 |
|
| 2009 |
Samimy M, Kim JH, Kearney-Fischer M. Active control of noise in supersonic jets using plasma actuators Proceedings of the Asme Turbo Expo. 1: 97-107. DOI: 10.1115/GT2009-59456 |
0.796 |
|
| 2009 |
Adamovich IV, Choi I, Jiang N, Kim JH, Keshav S, Lempert WR, Mintusov E, Nishihara M, Samimy M, Uddi M. Plasma assisted ignition and high-speed flow control: Non-thermal and thermal effects Plasma Sources Science and Technology. 18. DOI: 10.1088/0963-0252/18/3/034018 |
0.434 |
|
| 2009 |
Kearney-Fischer M, Kim JH, Samimy M. Control of a high Reynolds number Mach 0.9 heated jet using plasma actuators Physics of Fluids. 21. DOI: 10.1063/1.3210771 |
0.809 |
|
| 2009 |
Malone J, Debiasi M, Little J, Samimy M. Analysis of the spectral relationships of cavity tones in subsonic resonant cavity flows Physics of Fluids. 21. DOI: 10.1063/1.3139270 |
0.31 |
|
| 2009 |
Little J, Nishihara M, Adamovich I, Samimy M. Separation control from the flap of a high-lift airfoil using DBD plasma actuators 47th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.355 |
|
| 2009 |
Kearney-Fischer M, Kim JH, Samimy M. Noise control of a high Reynolds number mach 0.9 heated jet using plasma actuators 15th Aiaa/Ceas Aeroacoustics Conference (30th Aiaa Aeroacoustics Conference). |
0.817 |
|
| 2009 |
Kim JH, Kearney-Fischer M, Samimy M, Gogineni S. Active noise control in jets from conical and contoured supersonic nozzles with plasma actuators 15th Aiaa/Ceas Aeroacoustics Conference (30th Aiaa Aeroacoustics Conference). |
0.813 |
|
| 2008 |
Kim K, Kasnakoǧlu C, Serrani A, Samimy M. Extremum-seeking control of subsonic cavity flow 46th Aiaa Aerospace Sciences Meeting and Exhibit. DOI: 10.2514/1.38180 |
0.38 |
|
| 2008 |
Caraballo E, Kasnakoglu C, Serrani A, Samimy M. Control Input Separation Methods for Reduced-Order Model-Based Feedback Flow Control Aiaa Journal. 46: 2306-2322. DOI: 10.2514/1.35428 |
0.369 |
|
| 2008 |
Kihwan K, Debiasi M, Schultz R, Serrani A, Samimy M. Dynamic compensation of a synthetic jetlike actuator for closed-loop cavity flow control Aiaa Journal. 46: 232-240. DOI: 10.2514/1.30095 |
0.396 |
|
| 2008 |
Kim JH, Samimy M. Effects of active control on the flow structure in a high Reynolds number supersonic jet 4th Aiaa Flow Control Conference. DOI: 10.1260/175682509788913344 |
0.572 |
|
| 2008 |
Thurow BS, Jiang N, Kim JH, Lempert W, Samimy M. Issues with measurements of the convective velocity of large-scale structures in the compressible shear layer of a free jet Physics of Fluids. 20. DOI: 10.1063/1.2926757 |
0.724 |
|
| 2008 |
Kastner J, Kim JH, Samimy M. Toward better understanding of far-field radiated noise mechanisms in a high Reynolds number Mach 0.9 axisymmetric jet 46th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.512 |
|
| 2008 |
Kearney-Fischer M, Kim JH, Samimy M. Control of a heated high Reynolds number Mach 0.9 jet using plasma actuators 4th Aiaa Flow Control Conference. |
0.785 |
|
| 2008 |
Kim JH, Adamovich I, Samimy M. Active noise control in a Mach 1.3 ideally-expanded jet with plasma actuators 46th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.461 |
|
| 2008 |
Samimy M, Snyder RM, Kim JH, Adamovich I, Nishihara M. Active control of supersonic jets operating in various flow regimes 46th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.45 |
|
| 2007 |
Samimy M, Kim J, Kastner J, Adamovich I, Utkin Y. Active Control of a Mach 0.9 Jet for Noise Mitigation Using Plasma Actuators Aiaa Journal. 45: 890-901. DOI: 10.2514/1.27499 |
0.534 |
|
| 2007 |
Caraballo E, Little J, Debiasi M, Samimy M. Development and implementation of an experimental-based reduced-order model for feedback control of subsonic cavity flows Journal of Fluids Engineering, Transactions of the Asme. 129: 813-824. DOI: 10.1115/1.2742724 |
0.422 |
|
| 2007 |
Utkin YG, Keshav S, Kim JH, Kastner J, Adamovich IV, Samimy M. Development and use of localized arc filament plasma actuators for high-speed flow control Journal of Physics D: Applied Physics. 40: 685-694. DOI: 10.1088/0022-3727/40/3/S06 |
0.504 |
|
| 2007 |
Little J, Debiasi M, Caraballo E, Samimy M. Effects of open-loop and closed-loop control on subsonic cavity flows Physics of Fluids. 19. DOI: 10.1063/1.2740302 |
0.434 |
|
| 2007 |
Samimy M, Debiasi M, Caraballo E, Serrani A, Yuan X, Little J, Myatt JH. Feedback control of subsonic cavity flows using reduced-order models Journal of Fluid Mechanics. 579: 315-346. DOI: 10.1017/S0022112007005204 |
0.418 |
|
| 2007 |
Samimy M, Kim JH, Kastner J, Adamovich I, Utkin Y. Active control of high-speed and high-Reynolds-number jets using plasma actuators Journal of Fluid Mechanics. 578: 305-330. DOI: 10.1017/S0022112007004867 |
0.562 |
|
| 2007 |
Kastner J, Kim JH, Samimy M. Correlation of large-scale structure dynamics and far-field radiated noise in a mach 0.9 jet Collection of Technical Papers - 45th Aiaa Aerospace Sciences Meeting. 15: 10062-10078. |
0.547 |
|
| 2007 |
Samimy M, Kim JH, Kastner J, Adamovich I. Noise mitigation in high speed and high reynolds number jets using plasma actuators 13th Aiaa/Ceas Aeroacoustics Conference (28th Aiaa Aeroacoustics Conference). |
0.524 |
|
| 2007 |
Kim JH, Kastner J, Adamovich I, Samimy M. Active control of high subsonic jets Collection of Technical Papers - 45th Aiaa Aerospace Sciences Meeting. 6: 3900-3914. |
0.434 |
|
| 2006 |
Hileman JI, Samimy M. Mach number effects on jet noise sources and radiation to shallow angles Aiaa Journal. 44: 1915-1918. DOI: 10.2514/1.19959 |
0.794 |
|
| 2006 |
Kastner J, Samimy M, Hileman J, Freund JB. Comparison of noise mechanisms in high and low reynolds number high-speed jets Aiaa Journal. 44: 2251-2258. DOI: 10.2514/1.18384 |
0.811 |
|
| 2006 |
Yan P, Debiasi M, Yuan X, Little J, Ozbay H, Samimy M. Experimental Study of Linear Closed-Loop Control of Subsonic Cavity Flow Aiaa Journal. 44: 929-938. DOI: 10.2514/1.14873 |
0.392 |
|
| 2006 |
Kastner J, Kim JH, Samimy M. Noise sources in controlled high reynolds number and high speed jets Collection of Technical Papers - 12th Aiaa/Ceas Aeroacoustics Conference. 5: 3278-3290. |
0.544 |
|
| 2006 |
Little J, Debiasi M, Samimy M. Flow structure in controlled and baseline subsonic cavity flows Collection of Technical Papers - 44th Aiaa Aerospace Sciences Meeting. 8: 5697-5714. |
0.334 |
|
| 2006 |
Blohm M, Lempert W, Samimy M, Thurow B. A study of convective velocity in supersonic jets using MHz rate imaging Collection of Technical Papers - 44th Aiaa Aerospace Sciences Meeting. 1: 569-585. |
0.425 |
|
| 2005 |
Thurow BS, Jiang N, Lempert WR, Samimy M. Development of megahertz-rate planar Doppler velocimetry for high-speed flows Aiaa Journal. 43: 500-511. DOI: 10.2514/1.7749 |
0.723 |
|
| 2005 |
Hileman JI, Thurow BS, Caraballo EJ, Samimy M. Large-scale structure evolution and sound emission in high-speed jets: Real-time visualization with simultaneous acoustic measurements Journal of Fluid Mechanics. 544: 277-307. DOI: 10.1017/S002211200500666X |
0.847 |
|
| 2005 |
Thurow BS, Blohm M, Lempert WR, Samimy M. High repetition rate planar velocity measurements in a Mach 2.0 compressible axisymmetric jet 43rd Aiaa Aerospace Sciences Meeting and Exhibit - Meeting Papers. 7287-7306. |
0.7 |
|
| 2005 |
Kastner J, Samimy M, Hileman J, Freund JB. Comparison of noise sources in high and low reynolds number high speed jets Collection of Technical Papers - 11th Aiaa/Ceas Aeroacoustics Conference. 5: 3628-3639. |
0.784 |
|
| 2004 |
Thurow B, Jiang N, Samimy M, Lempert W. Narrow-linewidth megahertz-rate pulse-burst laser for high-speed flow diagnostics. Applied Optics. 43: 5064-73. PMID 15468708 DOI: 10.1364/Ao.43.005064 |
0.634 |
|
| 2004 |
Debiasi M, Samimy M. Logic-Based Active Control of Subsonic Cavity Flow Resonance Aiaa Journal. 42: 1901-1909. DOI: 10.2514/1.4799 |
0.485 |
|
| 2004 |
Hileman J, Thurow B, Samimy M. Development and evaluation of a 3-D microphone array to locate individual acoustic sources in a high-speed jet Journal of Sound and Vibration. 276: 649-669. DOI: 10.1016/J.Jsv.2003.08.022 |
0.822 |
|
| 2004 |
Samimy M, Adamovich I, Webb B, Kastner J, Hileman J, Keshav S, Palm P. Development and characterization of plasma actuators for high-speed jet control Experiments in Fluids. 37: 577-588. DOI: 10.1007/S00348-004-0854-7 |
0.781 |
|
| 2004 |
Debiasi M, Samimy M. Logic-based active control of subsonic cavity flow resonance Aiaa Journal. 42: 1901-1909. |
0.338 |
|
| 2004 |
Kastner J, Hileman J, Samimy M. Exploring high-speed axisymmetric jet noise control using Hartmann tube fluidic actuators Aiaa Paper. 1997-2009. |
0.773 |
|
| 2004 |
Hileman J, Caraballo E, Thurow B, Samimy M. Differences in dynamics of an idealy expanded mach 1.3 jet during noise generation and relative quiet periods Collection of Technical Papers - 10th Aiaa/Ceas Aeroacoustics Conference. 3: 2389-2406. |
0.836 |
|
| 2004 |
Thurow B, Jiang N, Lempert W, Samimy M. MHZ rate planar doppler velocimetry in supersonic jets Aiaa Paper. 4549-4565. |
0.706 |
|
| 2003 |
Caraballo E, Samimy M, Scott J, Narayanan S, DeBonis J. Application of proper orthogonal decomposition to a supersonic axisymmetric jet Aiaa Journal. 41: 866-877. DOI: 10.2514/2.2022 |
0.453 |
|
| 2003 |
Thurow B, Samimy M, Lempert W. Compressibility effects on turbulence structures of axisymmetric mixing layers Physics of Fluids. 15: 1755-1765. DOI: 10.1063/1.1570829 |
0.748 |
|
| 2003 |
Kastner J, Samimy M. Effects of forcing frequency on the control of an impinging high-speed jet 41st Aerospace Sciences Meeting and Exhibit. |
0.422 |
|
| 2003 |
Debiasi M, Samimy M. An experimental study of the cavity flow for closed-loop flow control 33rd Aiaa Fluid Dynamics Conference and Exhibit. |
0.36 |
|
| 2003 |
Hileman J, Caraballo E, Samimy M. Simultaneous real-time flow visualizations and acoustic measurements on a tabbed mach 1.3 jet 9th Aiaa/Ceas Aeroacoustics Conference and Exhibit. |
0.798 |
|
| 2003 |
Hileman J, Caraballo E, Thurow B, Samimy M. Further exploration of noise sources in a Mach 1.3 jet 41st Aerospace Sciences Meeting and Exhibit. |
0.487 |
|
| 2002 |
Hileman J, Thurow B, Samimy M. Exploring Noise Sources Using Simultaneous Acoustic Measurements and Real-Time Flow Visualizations in Jets Aiaa Journal. 40: 2382-2392. DOI: 10.2514/2.1599 |
0.846 |
|
| 2002 |
Kastner J, Samimy M. Development and characterization of Hartmann tube fluidic actuators for high-speed flow control Aiaa Journal. 40: 1926-1934. DOI: 10.2514/2.1541 |
0.46 |
|
| 2002 |
Hileman J, Samimy M. Effects of vortex generating tabs on noise sources in an ideally expanded mach 1.3 jet 8th Aiaa/Ceas Aeroacoustics Conference and Exhibit. DOI: 10.1260/147547203322436935 |
0.805 |
|
| 2002 |
Thurow B, Hileman J, Lempert W, Samimy M. A technique for real-time visualization of flow structure in high-speed flows Physics of Fluids. 14: 3449-3452. DOI: 10.1063/1.1503802 |
0.805 |
|
| 2002 |
Kastner J, Samimy M. Development and characterization of Hartmann tube based fluidic actuators for high speed flow control 40th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.364 |
|
| 2002 |
Samimy M, Kastner J, Debiasi M. Control of high-speed impinging jets using hartmann tube fluidic actuators 1st Flow Control Conference. |
0.349 |
|
| 2002 |
Thurow B, Samimy M, Lempert W. Structure of a supersonic impinging rectangular jet via real-time optical diagnostics 32nd Aiaa Fluid Dynamics Conference and Exhibit. |
0.396 |
|
| 2002 |
Lempert WR, Jiang N, Samimy M. Development of molecular tagging velocimetry for high speed flows in micro systems 40th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.333 |
|
| 2002 |
Sethuram S, Samimy M, Lempert W. Planar doppler velocimetry in supersonic micro flows 40th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.43 |
|
| 2002 |
Hileman J, Thurow B, Samimy M. Acoustic source localization using a 3-D microphone array in a mach 1.3 Jet 40th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.816 |
|
| 2002 |
Thurow B, Hileman J, Samimy M, Lempert W. Compressibility effects on the growth and development of large-scale structures in an axisymmetric jet 40th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.73 |
|
| 2001 |
Lempert WR, Jiang N, Sethuram S, Samimy M. Molecular tagging velocimetry measurements in supersonic micro jets American Society of Mechanical Engineers, Micro-Electromechanical Systems Division Publication (Mems). 3: 699-704. DOI: 10.2514/2.1789 |
0.449 |
|
| 2001 |
Hileman J, Samimy M. Turbulence structures and the acoustic far field of a Mach 1.3 jet Aiaa Journal. 39: 1716-1727. DOI: 10.2514/2.1529 |
0.791 |
|
| 2001 |
Kim JH, Samimy M, Lee S. Effects of compression and expansion on turbulence intensity in supersonic boundary layers Aiaa Journal. 39: 1071-1077. DOI: 10.2514/2.1419 |
0.449 |
|
| 2001 |
Kerechanin CW, Samimy M, Kim JH. Effects of nozzle trailing edges on acoustic field of supersonic rectangular jet Aiaa Journal. 39: 1065-1070. DOI: 10.2514/2.1418 |
0.555 |
|
| 2001 |
Hileman J, Thurow B, Samimy M. An experimental effort on the connection of turbulence structures to far-field acoustic radiation in a mach 1.3 JET 7th Aiaa/Ceas Aeroacoustics Conference and Exhibit. |
0.786 |
|
| 2001 |
Hileman J, Thurow B, Samimy M. Determination of noise sources within a high-speed jet via simultaneous acoustic measurements and real-time flow visualization 39th Aerospace Sciences Meeting and Exhibit. |
0.507 |
|
| 2001 |
Thurow B, Hileman J, Samimy M, Lempert W. Progress towards a real-time quantitative measurement technique for high-speed flows 15th Aiaa Computational Fluid Dynamics Conference. |
0.66 |
|
| 2001 |
Thurow B, Hileman J, Samimy M, Lempert W. An in-depth investigation of large scale structures in a mach 13 axisymmetric jet 39th Aerospace Sciences Meeting and Exhibit. |
0.431 |
|
| 2001 |
Thurow B, Hileman J, Samimy M, Lempert W. A MHZ rate imaging system for study of turbulent and time evolving high speed flows Iciasf Record, International Congress On Instrumentation in Aerospace Simulation Facilities. 37-47. |
0.784 |
|
| 2001 |
Caraballo E, Samimy M, Narayanan S, DeBonis J, Scott J. Application of proper orthogonal decomposition to a high speed axisymmetric jet 15th Aiaa Computational Fluid Dynamics Conference. |
0.402 |
|
| 2000 |
Kim JH, Samimy M. On mixing enhancement via nozzle trailing-edge modifications in high-speed jets Aiaa Journal. 38: 935-937. DOI: 10.2514/2.1052 |
0.493 |
|
| 2000 |
Samimy M, Wernet MP. Review of planar multiple-component velocimetry in high-speed flows Aiaa Journal. 38: 553-574. DOI: 10.2514/2.1004 |
0.434 |
|
| 2000 |
Hileman J, Samimy M. An attempt to identify noise generating turbulent structures in a high speed axisymmetric jet 6th Aeroacoustics Conference and Exhibit. |
0.518 |
|
| 2000 |
Kim JH, Samimy M. The effects of density change on turbulence level in supersonic boundary layers 38th Aerospace Sciences Meeting and Exhibit. |
0.353 |
|
| 2000 |
Thurow B, Lempert W, Samimy M. MHz rate imaging of large-scale structures within a high speed axisymmetric jet 38th Aerospace Sciences Meeting and Exhibit. |
0.358 |
|
| 2000 |
Kerechanin CW, Samimy M, Kim JH. Effects of nozzle trailing edge modifications on noise radiation in a supersonic rectangular jet 38th Aerospace Sciences Meeting and Exhibit. |
0.457 |
|
| 1999 |
Kim JH, Samimy M. Mixing enhancement via nozzle trailing edge modifications in a high speed rectangular jet Physics of Fluids. 11: 2731-2742. DOI: 10.1063/1.870132 |
0.516 |
|
| 1999 |
Kim JH, Samimy M. On the stream wise vortices in trailing edge modified supersonic jets 37th Aerospace Sciences Meeting and Exhibit. |
0.397 |
|
| 1998 |
Clancy PS, Samimy M, Erskine WR. Planar doppler velocimetry: Three-component velocimetry in supersonic jets 36th Aiaa Aerospace Sciences Meeting and Exhibit. DOI: 10.2514/2.798 |
0.424 |
|
| 1998 |
Samimy M, Kim JH, Clancy PS, Martens S. Passive control of supersonic rectangular jets via nozzle trailing-edge modifications Aiaa Journal. 36: 1230-1239. DOI: 10.2514/2.504 |
0.586 |
|
| 1998 |
Arnette SA, Samimy M, Elliott GS. The effects of expansion on the turbulence structure of compressible boundary layers Journal of Fluid Mechanics. 367: 67-105. DOI: 10.1017/S0022112098001475 |
0.417 |
|
| 1998 |
Amette SA, Samimy M, Elliott GS. Two-component planar Doppler velocimetry in the compressible turbulent boundary layer Experiments in Fluids. 24: 323-332. DOI: 10.1007/S003480050179 |
0.409 |
|
| 1998 |
Samimy M. A review of planar multiple-component velocimetry in high speed flows 20th Aiaa Advanced Measurement and Ground Testing Technology Conference. |
0.352 |
|
| 1998 |
Kim JH, Samimy M, Erskine WR. Mixing enhancement with minimal thrust loss in a high speed rectangular jet 36th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.464 |
|
| 1997 |
Belovich VM, Samimy M. Mixing processes in a coaxial geometry with a central lobed mixer-nozzle Aiaa Journal. 35: 838-841. DOI: 10.2514/2.7455 |
0.534 |
|
| 1997 |
Milam DM, Samimy M, Martens S. Lobed Mixers Using Simultaneous Laser-Induced Fluorescence and Mie Scattering Journal of Propulsion and Power. 13: 445-448. DOI: 10.2514/2.5184 |
0.325 |
|
| 1997 |
Clancy PS, Samimy M. Two-component planar Doppler velocimetry in high speed flows Aiaa Journal. 35: 1729-1738. DOI: 10.2514/2.42 |
0.382 |
|
| 1997 |
Clancyf PS, Samimy M. Multiple-component velocimetry in high speed flows using planar doppler velocimetry 35th Aerospace Sciences Meeting and Exhibit. |
0.344 |
|
| 1997 |
Samimy M, Kirn JH, Clancy PS. Mixing enhancement in supersonic jets via nozzle trailing edge modifications 4th Shear Flow Control Conference. |
0.421 |
|
| 1997 |
Samimy M, Kirn JH, Clancy PS. Supersonic jet noise reduction and mixing enhancement through nozzle trailing edge modifications 35th Aerospace Sciences Meeting and Exhibit. |
0.481 |
|
| 1996 |
Glawe DD, Samimy M, Nejad AS, Chen TH. Effects of Nozzle geometry on parallel injection into a supersonic flow Journal of Propulsion and Power. 12: 1159-1168. DOI: 10.2514/3.24156 |
0.473 |
|
| 1996 |
Reeder MF, Samimy M, Elliott GS. Investigation of the effect of tabs on supersonic jets using advanced diagnostics Journal of Propulsion and Power. 12: 742-751. DOI: 10.2514/3.24097 |
0.43 |
|
| 1996 |
Belovich VM, Samimy M, Reeder MF. Dual stream axisymmetric mixing in the presence of axial vorticity Journal of Propulsion and Power. 12: 178-185. DOI: 10.2514/3.24008 |
0.501 |
|
| 1996 |
Elliott GS, Samimy M. Rayleigh scattering technique for simultaneous measurements of velocity and thermodynamic properties Aiaa Journal. 34: 2346-2352. DOI: 10.2514/3.13400 |
0.398 |
|
| 1996 |
Reeder MF, Samimy M. The evolution of a jet with vortex-generating tabs: Real-time visualization and quantitative measurements Journal of Fluid Mechanics. 311: 73-118. DOI: 10.1017/S0022112096002510 |
0.501 |
|
| 1996 |
Martens S, Samimy M, Milam DM. Mixing enhancement in supersonic jets via trailing edge modifications American Society of Mechanical Engineers, Fluids Engineering Division (Publication) Fed. 237: 485-490. |
0.41 |
|
| 1996 |
Clancy P, Kim JH, Samimy M. Planar doppler velocimetry in high speed flows 1996 Fluid Dynamics Conference. 1-18. |
0.329 |
|
| 1996 |
Arnette SA, Samimy M, Elliott GS. The effects of expansion regions on the turbulence structure of compressible boundary layers 34th Aerospace Sciences Meeting and Exhibit. |
0.316 |
|
| 1995 |
Arnette SA, Samimy M, Elliott GS. Structure of supersonic turbulent boundary layer after expansion regions Aiaa Journal. 33: 430-438. DOI: 10.2514/3.60007 |
0.377 |
|
| 1995 |
Elliott GS, Samimy M, Arnette SA. The characteristics and evolution of large-scale structures in compressible mixing layers Physics of Fluids. 7: 864-876. DOI: 10.1063/1.868609 |
0.395 |
|
| 1995 |
Reeder MF, Samimy M, Elliott GS. An investigation of the effect of tabs on jets using advanced diagnostics 33rd Aerospace Sciences Meeting and Exhibit. |
0.33 |
|
| 1994 |
Dawson JA, Samimy M, Arnette SA. Effects of Expansions on a Supersonic Boundary Layer: Surface Pressure Measurements Aiaa Journal. 32: 2169-2177. DOI: 10.2514/3.12274 |
0.374 |
|
| 1994 |
Zaman KBMQ, Reeder MF, Samimy M. Control of an axisymmetric jet using vortex generators Physics of Fluids. 6: 778-793. DOI: 10.1063/1.868316 |
0.499 |
|
| 1994 |
Samimy M, Arnette SA, Elliott GS. Streamwise structures in a turbulent supersonic boundary layer Physics of Fluids. 6: 1081-1083. DOI: 10.1063/1.868279 |
0.402 |
|
| 1994 |
Elliott GS, Samimy M, Arnette SA. A molecular filter based velocimetry technique for high speed flows Experiments in Fluids. 18: 107-118. DOI: 10.1007/Bf00209367 |
0.407 |
|
| 1993 |
Samimy M, Zaman KBMQ, Reeder MF. Effect of tabs on the flow and noise field of an axisymmetric jet Aiaa Journal. 31: 609-619. DOI: 10.2514/3.11594 |
0.576 |
|
| 1993 |
Glawe DD, Samimy M. Dispersion of solid particles in compressible mixing layers Journal of Propulsion and Power. 9: 83-89. DOI: 10.2514/3.11488 |
0.346 |
|
| 1993 |
Reeder MF, Samimy M. Evolution of an axisymmetric jet with vortex-generating tabs American Society of Mechanical Engineers, Fluids Engineering Division (Publication) Fed. 174: 1-6. |
0.395 |
|
| 1992 |
Elliott GS, Samimy M, Arnette SA. Study of compressible mixing layers using filtered Rayleigh scattering based visualizations Aiaa Journal. 30: 2567-2569. DOI: 10.2514/3.11267 |
0.34 |
|
| 1992 |
Samimy M, Elliott GS, Erwin DE. Shock Wave/Free Shear Layer Interaction International Journal of Turbo and Jet Engines. 9: 125-134. DOI: 10.1515/Tjj.1992.9.2.125 |
0.398 |
|
| 1992 |
Arnette SA, Samimy M, Elliott GS. On streamwise vortices in high Reynolds number supersonic axisymmetric jets Physics of Fluids A. 5: 187-202. DOI: 10.1063/1.858803 |
0.538 |
|
| 1992 |
Samimy M, Reeder MF, Elliott GS. Compressibility effects on large structures in free shear flows Physics of Fluids A. 4: 1251-1258. DOI: 10.1063/1.858243 |
0.343 |
|
| 1991 |
Samimy M, Lele SK. Motion of particles with inertia in a compressible free shear layer Physics of Fluids A. 3: 1915-1923. DOI: 10.1063/1.857921 |
0.329 |
|
| 1990 |
Samimy M, Abu-Hijleh BAK. Structure of a reattaching supersonic shear layer Aiaa Journal. 28: 969-970. DOI: 10.2514/3.25150 |
0.347 |
|
| 1990 |
Samimy M, Nejad AS, Langenfeld CA, Favaloro SC. Nonaxisymmetric instabilities in a dump combustor with a swirling inlet flow Journal of Propulsion and Power. 6: 78-84. DOI: 10.2514/3.23226 |
0.44 |
|
| 1990 |
Samimy M, Elliott GS. Effects of compressibility on the characteristics of free shear layers Aiaa Journal. 28: 439-445. DOI: 10.2514/3.10412 |
0.419 |
|
| 1990 |
Elliott GS, Samimy M. Compressibility effects in free shear layers Physics of Fluids A. 2: 1231-1240. DOI: 10.1063/1.857816 |
0.448 |
|
| 1989 |
Samimy M, Abu-Hijleh BA. Performance of laser Doppler velocimeter with polydisperse seed particles in high-speed flows Journal of Propulsion and Power. 5: 21-25. DOI: 10.2514/3.23109 |
0.322 |
|
| 1989 |
Nejad AS, Vanka SP, Favaloro SC, Samimy M, Langenfeld C. Application of Laser Velocimetry for Characterization of Confined Swirling Flow Journal of Engineering For Gas Turbines and Power. 111: 36-45. DOI: 10.1115/1.3240225 |
0.453 |
|
| 1988 |
Samimy M, Langenfeld CA. Experimental study of isothermal swirling flows in a dump combustor Aiaa Journal. 26: 1442-1449. DOI: 10.2514/3.10062 |
0.463 |
|
| 1988 |
Petrie HL, Samimy M, Addy AL. Laser Doppler velocity bias in separated turbulent flows Exp. Fluids. 6. DOI: 10.1007/BF00196457 |
0.316 |
|
| 1986 |
Petrie HL, Samimy M, Addy AL. COMPRESSIBLE SEPARATED FLOWS Aiaa Journal. 24: 1971-1978. DOI: 10.2514/3.9555 |
0.473 |
|
| 1986 |
Samimy M, Addy AL. INTERACTION BETWEEN TWO COMPRESSIBLE, TURBULENT FREE SHEAR LAYERS Aiaa Journal. 24: 1918-1923. DOI: 10.2514/3.9548 |
0.446 |
|
| 1986 |
Samimy M, Addy AL. INTERACTION BETWEEN TWO COMPRESSIBLE TURBULENT FREE SHEAR LAYERS Aiaa Paper. |
0.312 |
|
| 1985 |
Samimy M, Petrie HL, Addy AL. STUDY OF COMPRESSIBLE TURBULENT REATTACHING FREE SHEAR LAYERS Aiaa Paper. DOI: 10.2514/3.9254 |
0.439 |
|
| 1985 |
Petrie HL, Samimy M, Addy AL. EVALUATION OF LDV VELOCITY AND FRINGE BIAS EFFECTS IN SEPARATED HIGH SPEED TURBULENT FLOWS Iciasf Record, International Congress On Instrumentation in Aerospace Simulation Facilities. 297-308. |
0.334 |
|
| 1985 |
Petrie HL, Samimy M, Addy AL. STUDY OF COMPRESSIBLE TURBULENT FREE SHEAR LAYERS USING LASER DOPPLER VELOCIMETRY Aiaa Paper. |
0.336 |
|
| 1983 |
Samimy M, Addy AL. The fluid dynamics of safety valve vent stacks . DOI: 10.1115/1.3242499 |
0.337 |
|
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