| Year |
Citation |
Score |
| 2021 |
Xiong Y, Smith EC, Conlon SC. Transmission loss of plates with embedded multi-scale and tuned acoustic black holes. The Journal of the Acoustical Society of America. 150: 2282. PMID 34598629 DOI: 10.1121/10.0006442 |
0.66 |
|
| 2020 |
Meng D, Xia P, Song L, Smith EC. Experimental Study on Piezoelectric-Stack-Actuator-Driven Active Vibration Control of Helicopter Floor Structure Journal of Aircraft. 57: 377-382. DOI: 10.2514/1.C035607 |
0.324 |
|
| 2020 |
Meng D, Xia P, Lang K, Smith EC, Rahn CD. Neural Network Based Hysteresis Compensation of Piezoelectric Stack Actuator Driven Active Control of Helicopter Vibration Sensors and Actuators a-Physical. 302: 111809. DOI: 10.1016/J.Sna.2019.111809 |
0.342 |
|
| 2019 |
Krott MJ, Smith EC, Rahn CD. Coupled and Multimode Tailboom Vibration Control Using Fluidic Flexible Matrix Composite Tubes Journal of the American Helicopter Society. 64: 1-10. DOI: 10.4050/Jahs.64.042007 |
0.346 |
|
| 2019 |
Miura K, Krott MJ, Smith EC, Rahn CD, Romano PQ. Experimental Demonstration of a Vibration Absorber Using Braid-Sheathed Fluidic Flexible Matrix Composite Tubes Journal of the American Helicopter Society. 64: 1-6. DOI: 10.4050/Jahs.64.032006 |
0.36 |
|
| 2017 |
Kambampati S, Smith EC. Aeroelastic optimization of high-speed tiltrotor wings with wing extensions and winglets Journal of Aircraft. 54: 1718-1727. DOI: 10.2514/1.C034195 |
0.312 |
|
| 2015 |
Wozniak MV, Conlon SC, Smith EC, Reichard KM. Design, analysis, and characterization of single crystal energy harvesters for rotorcraftwireless sensor applications Journal of the American Helicopter Society. 60. DOI: 10.4050/Jahs.60.022006 |
0.663 |
|
| 2015 |
Henry TC, Bakis CE, Smith EC. Viscoelastic characterization and self-heating behavior of laminated fiber composite driveshafts Materials and Design. 66: 346-355. DOI: 10.1016/J.Matdes.2014.10.083 |
0.302 |
|
| 2015 |
Henry TC, Bakis CE, Miller SW, Smith EC. Multi-objective optimal design of composite rotorcraft driveshaft including strain rate and temperature effects Composite Structures. 128: 42-53. DOI: 10.1016/J.Compstruct.2015.03.029 |
0.307 |
|
| 2013 |
Romano PQ, Conlon SC, Smith EC. Investigation of contact acoustic nonlinearities on metal and composite airframe structures via intensity based health monitoring. The Journal of the Acoustical Society of America. 133: 186-200. PMID 23297894 DOI: 10.1121/1.4770237 |
0.68 |
|
| 2013 |
Lewicki DG, DeSmidt H, Smith EC, Bauman SW. Dynamics of a dual-clutch gearbox system: Analysis and experimental validation Journal of the American Helicopter Society. 58. DOI: 10.4050/Jahs.58.012004 |
0.304 |
|
| 2013 |
Han D, Wang J, Smith EC, Lesieutre GA. Transient loads control of a variable speed rotor during lagwise resonance crossing Aiaa Journal. 51: 20-29. DOI: 10.2514/1.J050598 |
0.347 |
|
| 2013 |
Lotfi-Gaskarimahalle A, Scarborough LH, Rahn CD, Smith EC. Tunable fluidic composite mounts for vibration absorption Jvc/Journal of Vibration and Control. 20: 2137-2145. DOI: 10.1177/1077546313482340 |
0.356 |
|
| 2013 |
Han D, Smith EC. Lagwise dynamic analysis of a variable speed rotor Aerospace Science and Technology. 29: 277-286. DOI: 10.1016/J.Ast.2013.03.010 |
0.326 |
|
| 2012 |
Scarborough LH, Rahn CD, Smith EC. Fluidic composite tunable vibration isolators Journal of Vibration and Acoustics, Transactions of the Asme. 134. DOI: 10.1115/1.4004670 |
0.335 |
|
| 2012 |
Lotfi-Gaskarimahalle A, Scarborough LH, Rahn CD, Smith EC. Passive and switched stiffness vibration controllers using fluidic flexible matrix composites Journal of Vibration and Acoustics, Transactions of the Asme. 134. DOI: 10.1115/1.4002957 |
0.331 |
|
| 2009 |
Han D, Smith EC. Lagwise loads analysis of a rotor blade with an embedded chordwise absorber Journal of Aircraft. 46: 1280-1290. DOI: 10.2514/1.40569 |
0.36 |
|
| 2009 |
Semperlotti F, Wang KW, Smith EC. Localization of a Breathing Crack Using Super-Harmonic Signals due to System Nonlinearity Aiaa Journal. 47: 2076-2086. DOI: 10.2514/1.38947 |
0.609 |
|
| 2009 |
Semperlotti F, Wang KW, Smith EC. Localization of a breathing crack using nonlinear subharmonic response signals Applied Physics Letters. 95: 254101. DOI: 10.1063/1.3275705 |
0.591 |
|
| 2008 |
DeSmidt HA, Wang KW, Smith EC. Robust-adaptive magnetic bearing control of flexible matrix composite rotorcraft driveline Journal of the American Helicopter Society. 53: 115-124. DOI: 10.4050/Jahs.53.115 |
0.511 |
|
| 2008 |
DeSmidt HA, Wang KW, Smith EC. Multiharmonic adaptive vibration control of misaligned driveline via active magnetic bearings Journal of Dynamic Systems, Measurement and Control, Transactions of the Asme. 130: 0410061-04100613. DOI: 10.1115/1.2907382 |
0.345 |
|
| 2007 |
Kim J, Wang K, Smith E. Synthesis and Control of Piezoelectric Resonant Actuation Systems with Buckling-Beam Motion Amplifier Aiaa Journal. 46: 787-791. DOI: 10.2514/1.32216 |
0.522 |
|
| 2007 |
Kim J-, Wang KW, Smith EC. Development of a resonant trailing-edge flap actuation system for helicopter rotor vibration control Smart Materials and Structures. 16: 2275-2285. DOI: 10.1088/0964-1726/16/6/030 |
0.363 |
|
| 2006 |
Kang H, Smith EC, Lesieutre GA. Experimental and analytical study of blade lag damping augmentation using chordwise absorbers Journal of Aircraft. 43: 194-200. DOI: 10.2514/1.17074 |
0.367 |
|
| 2005 |
Desmidt HA, Wang KW, Smith EC, Provenza AJ. On the robust stability of segmented driveshafts with active magnetic bearing control Jvc/Journal of Vibration and Control. 11: 317-329. DOI: 10.1177/1077546305051200 |
0.339 |
|
| 2005 |
Kim JS, Wang KW, Smith EC. High-authority Piezoelectric Actuation System Synthesis through Mechanical Resonance and Electrical Tailoring Journal of Intelligent Material Systems and Structures. 16: 21-31. DOI: 10.1177/1045389X05046686 |
0.309 |
|
| 2004 |
Heverly DE, Wang KW, Smith EC. Dual-stack piezoelectric device with bidirectional actuation and improved performance Journal of Intelligent Material Systems and Structures. 15: 565-574. DOI: 10.1177/1045389X04044450 |
0.302 |
|
| 2004 |
DeSmidt HA, Wang KW, Smith EC. Stability of a segmented supercritical driveline with non-constant velocity couplings subjected to misalignment and torque Journal of Sound and Vibration. 277: 895-918. DOI: 10.1016/J.Jsv.2003.09.033 |
0.338 |
|
| 2004 |
Ramrakhyani DS, Lesieutre GA, Smith EC. Modeling of elastomeric materials using nonlinear fractional derivative and continuously yielding friction elements International Journal of Solids and Structures. 41: 3929-3948. DOI: 10.1016/J.Ijsolstr.2004.02.034 |
0.322 |
|
| 2003 |
Keller JA, Smith EC. Active Control of Gimballed Rotors Using Swashplate Actuation During Shipboard Engagement Operations Journal of Aircraft. 40: 726-733. DOI: 10.2514/2.3151 |
0.317 |
|
| 2003 |
Szefi JT, Smith EC, Lesieutre GA. Formulation and validation of a Ritz-based analytical model of high-frequency periodically layered isolators in compression Journal of Sound and Vibration. 268: 85-101. DOI: 10.1016/S0022-460X(02)01574-2 |
0.305 |
|
| 2002 |
DeSmidt HA, Wang KW, Smith EC. Coupled torsion-lateral stability of a shaft-disk system driven throuoh a universal joint Journal of Applied Mechanics, Transactions Asme. 69: 261-273. DOI: 10.1115/1.1460907 |
0.36 |
|
| 2002 |
Centolanza LR, Smith EC, Munsky B. Induced-shear piezoelectric actuators for rotor blade trailing edge flaps Smart Materials and Structures. 11: 24-35. DOI: 10.1088/0964-1726/11/1/303 |
0.337 |
|
| 2001 |
Heverly DE, Wang KW, Smith EC. An optimal actuator placement methodology for active control of helicopter airframe vibrations Journal of the American Helicopter Society. 46: 251-261. DOI: 10.4050/Jahs.46.251 |
0.324 |
|
| 2000 |
Brackbill CR, Lesieutre GA, Smith EC, Ruhl LE. Characterization and modeling of the low strain amplitude and frequency dependent behavior of elastomeric damper materials Journal of the American Helicopter Society. 45: 34-42. DOI: 10.4050/Jahs.45.34 |
0.357 |
|
| 1999 |
Keller JA, Smith EC. Experimental and Theoretical Correlation of Helicopter Rotor Blade-Droop Stop Impacts Journal of Aircraft. 36: 443-450. DOI: 10.2514/2.2450 |
0.353 |
|
| 1998 |
Geyer WP, Smith EC, Keller JA. Aeroelastic Analysis of Transient Blade Dynamics During Shipboard Engage/Disengage Operations Journal of Aircraft. 35: 445-453. DOI: 10.2514/2.2317 |
0.337 |
|
| 1996 |
Smith EC, Govindswamy K, Beale MR, Lesieutre GA. Formulation, validation, and application of a finite element model for elastomeric lag dampers Journal of the American Helicopter Society. 41: 247-256. DOI: 10.4050/Jahs.41.247 |
0.328 |
|
| 1994 |
Smith EC. Vibration and flutter of stiff-inplane elastically tailored composite rotor blades Mathematical and Computer Modelling. 19: 27-45. DOI: 10.1016/0895-7177(94)90055-8 |
0.365 |
|
| 1993 |
Smith EC, Chopra I. Air and ground resonance of helicopters with elastically tailored composite rotor blades Journal of the American Helicopter Society. 38: 50-61. DOI: 10.4050/Jahs.38.50 |
0.32 |
|
| 1993 |
Smith EC, Chopra I. Aeroelastic response, loads, and stability of a composite rotor in forward flight Aiaa Journal. 31: 1265-1273. DOI: 10.2514/3.49066 |
0.352 |
|
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