| Year |
Citation |
Score |
| 2010 |
Lee BH, Choo JH, Na S, Marzocca P, Librescu L. Sliding mode robust control of supersonic three degrees-of-freedom airfoils International Journal of Control, Automation and Systems. 8: 279-288. DOI: 10.1007/S12555-010-0214-8 |
0.575 |
|
| 2009 |
Qin Z, Hasanyan D, Librescu L. Electroconductive cylindrical thin elastic shells carrying electric current and immersed in a magnetic field: Implications of the current-magnetic coupling on the shells' instability International Journal of Applied Electromagnetics and Mechanics. 31: 79-96. DOI: 10.3233/Jae-2009-1049 |
0.585 |
|
| 2009 |
Yoon I, Song O, Librescu L. Vibration control of composite spacecraft booms subjected to solar heating Journal of Thermal Stresses. 32: 95-111. DOI: 10.1080/01495730802540742 |
0.464 |
|
| 2009 |
Na S, Yoon GC, Lee BH, Marzocca P, Librescu L. Dynamic response control of rotating composite booms under solar radiation Journal of Thermal Stresses. 32: 21-40. DOI: 10.1080/01495730802540205 |
0.654 |
|
| 2009 |
Librescu L, Maalawi KY. Aeroelastic design optimization of thin-walled subsonic wings against divergence Thin-Walled Structures. 47: 89-97. DOI: 10.1016/J.Tws.2008.05.007 |
0.401 |
|
| 2008 |
Polli GM, Mastroddi F, Librescu L, Trapani CD. Aerothermoelastic Stability of Composite Aerovehicle Wings Subjected to Heat Inputs Aiaa Journal. 46: 992-1001. DOI: 10.2514/1.32397 |
0.418 |
|
| 2008 |
Librescu L, Song O. Dynamics of Composite Aircraft Wings Carrying External Stores Aiaa Journal. 46: 568-577. DOI: 10.2514/1.25541 |
0.495 |
|
| 2008 |
Hasanyan D, Qin Z, Librescu L. Elastic Stress and Magnetic Field Concentration Near the Vertex of a Soft-Ferromagnetic 2D Compound Wedge Journal of Applied Mechanics. 75: 41013. DOI: 10.1115/1.2912937 |
0.583 |
|
| 2008 |
Librescu L, Na S, Qin Z, Lee B. Active aeroelastic control of aircraft composite wings impacted by explosive blasts Journal of Sound and Vibration. 318: 74-92. DOI: 10.1016/J.Jsv.2008.04.007 |
0.492 |
|
| 2008 |
Hohe J, Librescu L. Recent results on the effect of the transverse core compressibility on the static and dynamic response of sandwich structures Composites Part B-Engineering. 39: 108-119. DOI: 10.1016/J.Compositesb.2007.02.007 |
0.463 |
|
| 2008 |
Librescu L, Oh S, Song O, Kang H. Dynamics of advanced rotating blades made of functionally graded materials and operating in a high-temperature field Journal of Engineering Mathematics. 61: 1-16. DOI: 10.1007/S10665-007-9155-5 |
0.437 |
|
| 2007 |
Hause T, Librescu L. Doubly Curved Anisotropic Sandwich Panels: Modeling and Free Vibration Journal of Aircraft. 44: 1327-1336. DOI: 10.2514/1.26990 |
0.371 |
|
| 2007 |
Qin Z, Librescu L, Hasanyan D. Joule Heating and its Implications on Crack Detection/Arrest in Electrically Conductive Circular Cylindrical Shells Journal of Thermal Stresses. 30: 623-637. DOI: 10.1080/01495730701274245 |
0.573 |
|
| 2007 |
Song O, Kwon HD, Librescu L. Modelling and vibration of a non-classical tilt-rotor wing system Aeronautical Journal. 111: 285-295. DOI: 10.1017/S000192400000453X |
0.414 |
|
| 2007 |
Yu P, Chen Z, Librescu L, Marzocca P. Implications of time-delayed feedback control on limit cycle oscillation of a two-dimensional supersonic lifting surface Journal of Sound and Vibration. 304: 974-986. DOI: 10.1016/J.Jsv.2007.03.030 |
0.622 |
|
| 2007 |
Hause T, Librescu L. Dynamic response of doubly-curved anisotropic sandwich panels impacted by blast loadings International Journal of Solids and Structures. 44: 6678-6700. DOI: 10.1016/J.Ijsolstr.2007.03.006 |
0.426 |
|
| 2007 |
Na SS, Librescu L, Marzocca P, Yoon GC, Rubillo C, Bong K. Robust aeroelastic control of two-dimensional supersonic flapped wing systems Acta Mechanica. 192: 37-47. DOI: 10.1007/S00707-006-0419-3 |
0.607 |
|
| 2006 |
Na S, Librescu L, Kim MH, Jeong IJ, Marzocca P. Aeroelastic response of flapped-wing systems using robust estimation control methodology Journal of Guidance, Control, and Dynamics. 29: 199-203. DOI: 10.2514/1.15015 |
0.571 |
|
| 2006 |
Na SS, Librescu L, Rim SN, Yoon GC. Vibration and Dynamic Response Control of Nonuniform Composite Rotating Blades International Journal of Rotating Machinery. 2006: 13807. DOI: 10.1155/Ijrm/2006/13807 |
0.477 |
|
| 2006 |
Na SS, Yoon H, Librescu L. Effect of taper ratio on vibration and stability of a composite thin-walled spinning shaft Thin-Walled Structures. 44: 362-371. DOI: 10.1016/J.Tws.2006.02.007 |
0.413 |
|
| 2006 |
Hause T, Librescu L. Flexural free vibration of sandwich flat panels with laminated anisotropic face sheets Journal of Sound and Vibration. 297: 823-841. DOI: 10.1016/J.Jsv.2006.04.024 |
0.366 |
|
| 2006 |
Hasanyan DJ, Librescu L, Ambur DR. Buckling and postbuckling of magnetoelastic flat plates carrying an electric current International Journal of Solids and Structures. 43: 4971-4996. DOI: 10.1016/J.Ijsolstr.2005.04.028 |
0.421 |
|
| 2006 |
Hohe J, Librescu L, Oh SY. Dynamic buckling of flat and curved sandwich panels with transversely compressible core Composite Structures. 74: 10-24. DOI: 10.1016/J.Compstruct.2005.03.003 |
0.46 |
|
| 2006 |
Na S, Librescu L, Kim MH, Jeong IJ, Marzocca P. Robust aeroelastic control of flapped wing systems using a sliding mode observer Aerospace Science and Technology. 10: 120-126. DOI: 10.1016/J.Ast.2005.10.002 |
0.336 |
|
| 2006 |
Librescu L, Oh S, Hohe J. Dynamic response of anisotropic sandwich flat panels to underwater and in-air explosions International Journal of Solids and Structures. 43: 3794-3816. DOI: 10.1007/1-4020-3848-8_9 |
0.418 |
|
| 2005 |
Marzocca P, Librescu L, Silva WA. Time-Delay Effects on Linear/Nonlinear Feedback Control of Simple Aeroelastic Systems Journal of Guidance Control and Dynamics. 28: 53-62. DOI: 10.2514/1.4335 |
0.587 |
|
| 2005 |
Marzocca P, Librescu L, Kim D, Lee I, Schober S. Generalized Transonic Unsteady Aerodynamics via Computational-Fluid-Dynamics/ Indicial Approach. Aiaa Journal. 43: 915-917. DOI: 10.2514/1.3634 |
0.533 |
|
| 2005 |
Ambur DR, Hasanyan D, Librescu L, Qin Z. Diffraction of harmonic flexural waves in a cracked elastic plate carrying electrical current Proceedings of the Royal Society a: Mathematical, Physical and Engineering Sciences. 461: 3543-3560. DOI: 10.1098/Rspa.2005.1512 |
0.598 |
|
| 2005 |
Librescu L, Oh S, Song O. Thin-Walled Beams Made of Functionally Graded Materials and Operating in a High Temperature Environment: Vibration and Stability Journal of Thermal Stresses. 28: 649-712. DOI: 10.1080/01495730590934038 |
0.421 |
|
| 2005 |
Hasanyan D, Librescu L, Qin Z. Thermoelastic Cracked Plates Carrying Nonstationary Electrical Current Journal of Thermal Stresses. 28: 729-745. DOI: 10.1080/01495730590932715 |
0.572 |
|
| 2005 |
Oh S-, Librescu L, Song O. Modelling and vibration of composite thin-walled rotating blades featuring extension-twist elastic coupling Aeronautical Journal. 109: 233-246. DOI: 10.1017/S0001924000005212 |
0.413 |
|
| 2005 |
Qin Z, Hasanyan D, Librescu L, Ambur DR. Magneto-thermo-elastokinetics of geometrically nonlinear laminated composite plates. Part 2: vibration and wave propagation Journal of Sound and Vibration. 287: 177-201. DOI: 10.1016/J.Jsv.2004.10.053 |
0.665 |
|
| 2005 |
Hasanyan D, Librescu L, Qin Z, Ambur DR. Magneto-thermo-elastokinetics of Geometrically Nonlinear Laminated Composite Plates. Part 1: Foundation of the Theory Journal of Sound and Vibration. 287: 153-175. DOI: 10.1016/J.Jsv.2004.10.050 |
0.667 |
|
| 2005 |
Oh S, Librescu L, Song O. Vibration and instability of functionally graded circular cylindrical spinning thin-walled beams Journal of Sound and Vibration. 285: 1071-1091. DOI: 10.1016/J.Jsv.2004.09.018 |
0.42 |
|
| 2005 |
Librescu L, Na S, Marzocca P, Chung C, Kwak MK. Active aeroelastic control of 2-D wing-flap systems operating in an incompressible flowfield and impacted by a blast pulse Journal of Sound and Vibration. 283: 685-706. DOI: 10.1016/J.Jsv.2004.05.010 |
0.555 |
|
| 2005 |
Librescu L, Marzocca P, Silva WA. Aeroelasticity of 2-D lifting surfaces with time-delayed feedback control Journal of Fluids and Structures. 20: 197-215. DOI: 10.1016/J.Jfluidstructs.2004.10.005 |
0.593 |
|
| 2005 |
Hause T, Librescu L. Dynamic response of anisotropic sandwich flat panels to explosive pressure pulses International Journal of Impact Engineering. 31: 607-628. DOI: 10.1016/J.Ijimpeng.2004.01.002 |
0.384 |
|
| 2005 |
Librescu L, Na S. Comparative study on vibration control methodologies applied to adaptive thin-walled anisotropic cantilevers European Journal of Mechanics, a/Solids. 24: 661-675. DOI: 10.1016/J.Euromechsol.2004.12.006 |
0.437 |
|
| 2005 |
Hasanyan D, Librescu L, Qin Z, Ambur DR. Nonlinear vibration of finitely-electroconductive plate strips in an axial magnetic field Computers & Structures. 83: 1205-1216. DOI: 10.1016/J.Compstruc.2004.08.027 |
0.652 |
|
| 2005 |
Librescu L, Marzocca P. Advances in the linear/nonlinear control of aeroelastic structural systems Acta Mechanica. 178: 147-186. DOI: 10.1007/S00707-005-0222-6 |
0.611 |
|
| 2005 |
Hohe J, Librescu L. Transient dynamic response of sandwich shells with transversely compressible core Pamm. 5: 235-236. DOI: 10.1002/Pamm.200510095 |
0.415 |
|
| 2004 |
Marzocca P, Silva WA, Librescu L. Nonlinear Open-/Closed-Loop Aeroelastic Analysis of Airfoils via Volterra Series Aiaa Journal. 42: 673-686. DOI: 10.2514/1.9552 |
0.62 |
|
| 2004 |
Na SS, Librescu L, Shim JH. Modified bang-bang vibration control applied to adaptive thin-walled beam cantilevers Aiaa Journal. 42: 1717-1721. DOI: 10.2514/1.831 |
0.384 |
|
| 2004 |
Librescu L, Marzocca P, Silva WA. Linear/Nonlinear Supersonic Panel Flutter in a High-Temperature Field Journal of Aircraft. 41: 918-924. DOI: 10.2514/1.679 |
0.616 |
|
| 2004 |
Yuan Y, Yu P, Librescu L, Marzocca P. Aeroelasticity of Time-Delayed Feedback Control of Two-Dimensional Supersonic Lifting Surfaces Journal of Guidance Control and Dynamics. 27: 795-803. DOI: 10.2514/1.3445 |
0.606 |
|
| 2004 |
Polli GM, Librescu L, Mastroddi F. Aeroelastic response of composite aircraft swept wings impacted by a laser beam Aiaa Journal. 44: 382-391. DOI: 10.2514/1.15930 |
0.429 |
|
| 2004 |
Hohe J, Librescu L. Advances in the Structural Modeling of Elastic Sandwich Panels Mechanics of Advanced Materials and Structures. 11: 395-424. DOI: 10.1080/15376490490451561 |
0.351 |
|
| 2004 |
Na SS, Librescu L, Jung H. Dynamics And Active Bending Vibration Control Of Turbomachinery Rotating Blades Featuring Temperature-Dependent Material Properties Journal of Thermal Stresses. 27: 625-644. DOI: 10.1080/01495730490466219 |
0.454 |
|
| 2004 |
Librescu L, Hasanyan D, Ambur DR. Electromagnetically conducting elastic plates in a magnetic field: modeling and dynamic implications International Journal of Non-Linear Mechanics. 39: 723-739. DOI: 10.1016/S0020-7462(03)00023-4 |
0.412 |
|
| 2004 |
Hasanyan DJ, Librescu L, Ambur DR. A few results on the foundation of the theory and behavior of nonlinear magnetoelastic plates carrying an electrical current International Journal of Engineering Science. 42: 1547-1572. DOI: 10.1016/J.Ijengsci.2004.04.003 |
0.425 |
|
| 2004 |
Librescu L, Oh SY, Song O. Spinning thin-walled beams made of functionally graded materials: modeling, vibration and instability European Journal of Mechanics a-Solids. 23: 499-515. DOI: 10.1016/J.Euromechsol.2003.12.003 |
0.408 |
|
| 2004 |
Librescu L, Oh S, Hohe J. Linear and non-linear dynamic response of sandwich panels to blast loading Composites Part B-Engineering. 35: 673-683. DOI: 10.1016/J.Compositesb.2003.07.003 |
0.429 |
|
| 2003 |
Qin Z, Librescu L, Marzocca P. Aeroelasticity of composite aerovehicle wings in supersonic flows Journal of Spacecraft and Rockets. 40: 162-173. DOI: 10.2514/2.3950 |
0.746 |
|
| 2003 |
Qin Z, Librescu L. Dynamic Aeroelastic Response of Aircraft Wings Modeled as Anisotropic Thin-Walled Beams Journal of Aircraft. 40: 532-543. DOI: 10.2514/2.3127 |
0.687 |
|
| 2003 |
Oh S, Librescu L, Song O. Thermoelastic Modeling and Vibration of Functionally Graded Thin-Walled Rotating Blades Aiaa Journal. 41: 2051-2061. DOI: 10.2514/2.1897 |
0.429 |
|
| 2003 |
Hohe J, Librescu L. Core and Face-Sheet Anisotropy in Deformation and Buckling of Sandwich Panels Aiaa Journal. 42: 149-158. DOI: 10.2514/1.1203 |
0.376 |
|
| 2003 |
Librescu L, Hasanyan D, Qin Z, Ambur DR. Nonlinear magnetothermoelasticity of anisotropic plates immersed in a magnetic field Journal of Thermal Stresses. 26: 1277-1304. DOI: 10.1080/714050886 |
0.656 |
|
| 2003 |
Qin Z, Librescu L. Aeroelastic instability of aircraft wings modelled as anisotropic composite thin-walled beams in incompressible flow Journal of Fluids and Structures. 18: 43-61. DOI: 10.1016/S0889-9746(03)00082-3 |
0.469 |
|
| 2003 |
Hohe J, Librescu L. A nonlinear theory for doubly curved anisotropic sandwich shells with transversely compressible core International Journal of Solids and Structures. 40: 1059-1088. DOI: 10.1016/S0020-7683(02)00656-X |
0.449 |
|
| 2003 |
Oh S-, Song O, Librescu L. Effects of pretwist and presetting on coupled bending vibrations of rotating thin-walled composite beams International Journal of Solids and Structures. 40: 1203-1224. DOI: 10.1016/S0020-7683(02)00605-4 |
0.462 |
|
| 2003 |
Librescu L, Chiocchia G, Marzocca P. Implications of cubic physical/aerodynamic non-linearities on the character of the flutter instability boundary International Journal of Non-Linear Mechanics. 38: 173-199. DOI: 10.1016/S0020-7462(01)00054-3 |
0.591 |
|
| 2003 |
Qin Z, Hasanyan D, Librescu L, Ambur DR. Magnetoelastic modeling of circular cylindrical shells immersed in a magnetic field: Part II: Implications of finite dimensional effects on the free vibrations International Journal of Engineering Science. 41: 2023-2046. DOI: 10.1016/S0020-7225(03)00135-6 |
0.663 |
|
| 2003 |
Qin Z, Librescu L, Hasanyan D, Ambur DR. Magnetoelastic modeling of circular cylindrical shells immersed in a magnetic field. Part I: Magnetoelastic loads considering finite dimensional effects International Journal of Engineering Science. 41: 2005-2022. DOI: 10.1016/S0020-7225(03)00134-4 |
0.638 |
|
| 2003 |
Librescu L, Qin Z, Ambur DR. Implications of warping restraint on statics and dynamics of elastically tailored thin-walled composite beams International Journal of Mechanical Sciences. 45: 1247-1267. DOI: 10.1016/J.Ijmecsci.2003.10.003 |
0.661 |
|
| 2003 |
Na S, Librescu L, Shim JK. Modeling and bending vibration control of nonuniform thin-walled rotating beams incorporating adaptive capabilities International Journal of Mechanical Sciences. 45: 1347-1367. DOI: 10.1016/J.Ijmecsci.2003.09.015 |
0.474 |
|
| 2003 |
Oh S-, Librescu L, Song O. Vibration of turbomachinery rotating blades made-up of functionally graded materials and operating in a high temperature field Acta Mechanica. 166: 69-87. DOI: 10.1007/S00707-003-0049-Y |
0.384 |
|
| 2003 |
Hohe J, Librescu L. A Nonlinear Sandwich Shell Theory Accounting for Transverse Core Compressibility Pamm. 2: 158-159. DOI: 10.1002/Pamm.200310064 |
0.428 |
|
| 2002 |
Marzocca P, Librescu L, Silva WA. Flutter, Postflutter, and Control of a Supersonic Wing Section Journal of Guidance Control and Dynamics. 25: 962-970. DOI: 10.2514/2.4970 |
0.604 |
|
| 2002 |
Librescu L, Marzocca P, Silva WA. Supersonic/Hypersonic Flutter and Postflutter of Geometrically Imperfect Circular Cylindrical Panels Journal of Spacecraft and Rockets. 39: 802-812. DOI: 10.2514/2.3882 |
0.64 |
|
| 2002 |
Na SS, Librescu L. Optimal dynamic response control of elastically tailored nonuniform thin-walled adaptive beams Journal of Aircraft. 39: 469-479. DOI: 10.2514/2.2952 |
0.459 |
|
| 2002 |
Marzocca P, Librescu L, Silva WA. Aeroelastic Response of Nonlinear Wing Sections Using a Functional Series Technique Aiaa Journal. 40: 813-824. DOI: 10.2514/2.1735 |
0.619 |
|
| 2002 |
Marzocca P, Librescu L, Silva WA. Aeroelastic Response and Flutter of Swept Aircraft Wings Aiaa Journal. 40: 801-812. DOI: 10.2514/2.1724 |
0.581 |
|
| 2002 |
Song O, Oh S, Librescu L. Dynamic Behavior of Elastically Tailored Rotating Blades Modeled as Pretwisted Thin-Walled Beams and Incorporating Adaptive Capabilities International Journal of Rotating Machinery. 8: 13-25. DOI: 10.1155/S1023621X02000027 |
0.444 |
|
| 2002 |
Chandiramani NK, Librescu L, Shete CD. On the free-vibration of rotating composite beams using a higher-order shear formulation Aerospace Science and Technology. 6: 545-561. DOI: 10.1016/S1270-9638(02)01195-1 |
0.498 |
|
| 2002 |
Marzocca P, Librescu L, Chiocchia G. Aeroelastic response of a 2-D airfoil in a compressible flow field and exposed to blast loading Aerospace Science and Technology. 6: 259-272. DOI: 10.1016/S1270-9638(02)01169-0 |
0.615 |
|
| 2002 |
Qin Z, Marzocca P, Librescu L. Aeroelastic instability and response of advanced aircraft wings at subsonic flight speeds Aerospace Science and Technology. 6: 195-208. DOI: 10.1016/S1270-9638(02)01158-6 |
0.752 |
|
| 2002 |
Qin Z, Librescu L. On a shear-deformable theory of anisotropic thin-walled beams: further contribution and validations Composite Structures. 56: 345-358. DOI: 10.1016/S0263-8223(02)00019-3 |
0.68 |
|
| 2002 |
Sciuva MD, Gherlone M, Librescu L. Implications of damaged interfaces and of other non-classical effects on the load carrying capacity of multilayered composite shallow shells International Journal of Non-Linear Mechanics. 37: 851-867. DOI: 10.1016/S0020-7462(01)00102-0 |
0.46 |
|
| 2002 |
Song O, Librescu L, Jeong N. Vibration And Stability Control Of Smart Composite Rotating Shaft Via Structural Tailoring And Piezoelectric Strain Actuation Journal of Sound and Vibration. 257: 503-525. DOI: 10.1006/Jsvi.2002.5050 |
0.444 |
|
| 2002 |
Song O, Librescu L, Kwon H. Vibration and stability control of robotic manipulator systems consisting of a thin‐walled beam and a spinning tip rotor Journal of Robotic Systems. 19: 469-482. DOI: 10.1002/Rob.10053 |
0.463 |
|
| 2001 |
Song O, Jeong NH, Librescu L. Implication of conservative and gyroscopic forces on vibration and stability of an elastically tailored rotating shaft modeled as a composite thin-walled beam. The Journal of the Acoustical Society of America. 109: 972-81. PMID 11303949 DOI: 10.1121/1.1348301 |
0.451 |
|
| 2001 |
Song O, Librescu L, Oh S. Vibration of pretwisted adaptive rotating blades modeled as anisotropic thin-walled beams Aiaa Journal. 39: 285-295. DOI: 10.2514/2.1303 |
0.465 |
|
| 2001 |
Qin Z, Librescu L. Static and Dynamic Validations of a Refined Thin-Walled Composite Beam Model Aiaa Journal. 39: 2422-2424. DOI: 10.2514/2.1259 |
0.637 |
|
| 2001 |
Song OS, Kwon H, Librescu L. Modeling, vibration, and stability of elastically tailored composite thin-walled beams carrying a spinning tip rotor Journal of the Acoustical Society of America. 110: 877-886. DOI: 10.1121/1.1377292 |
0.447 |
|
| 2001 |
Song O, Librescu L, Oh SY. Dynamics of pretwisted rotating thin-walled beams operating in a temperature environment Journal of Thermal Stresses. 24: 255-279. DOI: 10.1080/014957301300006407 |
0.426 |
|
| 2001 |
Sciuva MD, Librescu L. Contribution to the nonlinear theory of multilayered composite shells featuring damaged interfaces Composites Part B-Engineering. 32: 219-227. DOI: 10.1016/S1359-8368(00)00058-5 |
0.442 |
|
| 2001 |
Na S, Librescu L. Dynamic response of elastically tailored adaptive cantilevers of nonuniform cross section exposed to blast pressure pulses International Journal of Impact Engineering. 25: 847-867. DOI: 10.1016/S0734-743X(01)00022-7 |
0.446 |
|
| 2001 |
Marzocca P, Librescu L, Chiocchia G. Aeroelastic response of 2-D lifting surfaces to gust and arbitrary explosive loading signatures International Journal of Impact Engineering. 25: 41-65. DOI: 10.1016/S0734-743X(00)00033-6 |
0.603 |
|
| 2001 |
Librescu L, Na S. Active vibration control of doubly tapered thin-walled beams using piezoelectric actuation Thin-Walled Structures. 39: 65-82. DOI: 10.1016/S0263-8231(00)00054-9 |
0.463 |
|
| 2001 |
Song O, Librescu L, Jeong N. Static response of thin-walled composite I-beams loaded at their free-end cross-section: analytical solution Composite Structures. 52: 55-65. DOI: 10.1016/S0263-8223(00)00190-2 |
0.441 |
|
| 2001 |
Librescu L, Schmidt R. A general linear theory of laminated composite shells featuring interlaminar bonding imperfections International Journal of Solids and Structures. 38: 3355-3375. DOI: 10.1016/S0020-7683(00)00263-8 |
0.414 |
|
| 2001 |
Song O, Kim J, Librescu L. Synergistic implications of tailoring and adaptive materials technology on vibration control of anisotropic thin-walled beams International Journal of Engineering Science. 39: 71-94. DOI: 10.1016/S0020-7225(00)00029-X |
0.472 |
|
| 2000 |
Icardi U, Sciuva MD, Librescu L. Dynamic Response of Adaptive Cross-Ply Cantilevers Featuring Interlaminar Bonding Imperfections Aiaa Journal. 38: 499-506. DOI: 10.2514/2.988 |
0.415 |
|
| 2000 |
Na SS, Librescu L. Optimal Vibration Control of Thin-Walled Anisotropic Cantilevers Exposed to Blast Loadings Journal of Guidance Control and Dynamics. 23: 491-500. DOI: 10.2514/2.4555 |
0.413 |
|
| 2000 |
Hause T, Johnson TF, Librescu L. Effect of Face-Sheet Anisotropy on Buckling and Postbuckling of Sandwich Plates Journal of Spacecraft and Rockets. 37: 331-341. DOI: 10.2514/2.3583 |
0.432 |
|
| 2000 |
Gern FH, Librescu L. Aeroelastic Tailoring of Composite Wings Exhibiting Nonclassical Effects and Carrying External Stores Journal of Aircraft. 37: 1097-1104. DOI: 10.2514/2.2718 |
0.474 |
|
| 2000 |
Librescu L, Hause T, Johnson TF. Buckling and Nonlinear Response of Sandwich Curved Panels to Combined Mechanical Loads-Implications of Face-Sheet Elastic Tailoring Journal of Sandwich Structures and Materials. 2: 246-269. DOI: 10.1177/109963620000200305 |
0.441 |
|
| 2000 |
Na SS, Librescu L. Optimal Dynamic Response Control of Adaptive Thin-Walled Cantilevers Carrying Heavy Stores and Exposed to Blast Pulses Journal of Intelligent Material Systems and Structures. 11: 703-712. DOI: 10.1106/Ld1R-Whmw-Jp4K-Nqqx |
0.445 |
|
| 2000 |
Librescu L, Hause T. Recent developments in the modeling and behavior of advanced sandwich constructions: a survey Composite Structures. 48: 1-17. DOI: 10.1016/S0263-8223(99)00068-9 |
0.389 |
|
| 2000 |
Song O, Jeong N-, Librescu L. Vibration And Stability Of Pretwisted Spinning Thin-Walled Composite Beams Featuring Bending–Bending Elastic Coupling Journal of Sound and Vibration. 237: 513-533. DOI: 10.1006/Jsvi.2000.3100 |
0.448 |
|
| 2000 |
Na S, Librescu L. Dynamic response of adaptive cantilevers carrying external stores and subjected to blast loading Journal of Sound and Vibration. 231: 1039-1055. DOI: 10.1006/Jsvi.1999.2627 |
0.474 |
|
| 1999 |
Sciuva MD, Icardi U, Librescu L. Effects of interfacial damage on the global and local static response of cross-ply laminates International Journal of Fracture. 96: 17-35. DOI: 10.1023/A:1018649824301 |
0.486 |
|
| 1999 |
Librescu L, Lin W. Non-linear response of laminated plates and shells to thermomechanical loading: Implications of violation of interlaminar shear traction continuity requirement International Journal of Solids and Structures. 36: 4111-4147. DOI: 10.1016/S0020-7683(98)00185-1 |
0.472 |
|
| 1999 |
Song O, Librescu L. Modeling and dynamic behavior of rotating blades carrying a tip mass and incorporating adaptive capabilities Acta Mechanica. 134: 169-197. DOI: 10.1007/Bf01312654 |
0.464 |
|
| 1999 |
Chang M, Librescu L. Vibration Control Of Shear Deformable Laminated Plates—Modeling Implications Journal of Sound and Vibration. 228: 731-760. DOI: 10.1006/Jsvi.1999.2444 |
0.416 |
|
| 1998 |
Gern FH, Librescu L. Static and Dynamic Aeroelasticity of Advanced Aircraft Wings Carrying External Stores Aiaa Journal. 36: 1121-1129. DOI: 10.2514/2.499 |
0.468 |
|
| 1998 |
Librescu L, Na SS. Bending Vibration Control of Cantilevers via Boundary Moment and Combined Feedback Control Laws Journal of Vibration and Control. 4: 733-746. DOI: 10.1177/107754639800400605 |
0.463 |
|
| 1998 |
Na S, Librescu L. Oscillation control of cantilevers via smart materials technology and optimal feedback control: Actuator location and power consumption issues Smart Materials and Structures. 7: 833-842. DOI: 10.1088/0964-1726/7/6/011 |
0.391 |
|
| 1998 |
Hause T, Librescu L, Johnson TF. Thermomechanical load-carrying capacity of sandwich flat panels Journal of Thermal Stresses. 21: 627-653. DOI: 10.1080/01495739808956166 |
0.391 |
|
| 1998 |
Gern FH, Librescu L. Effects of externally mounted stores on aeroelasticity of advanced swept cantilevered aircraft wings Aerospace Science and Technology. 2: 321-333. DOI: 10.1016/S1270-9638(98)80008-4 |
0.466 |
|
| 1998 |
Librescu L, Na SS. Boundary control of free and forced oscillation of shearable thin-walled beam cantilevers European Journal of Mechanics a-Solids. 17: 687-700. DOI: 10.1016/S0997-7538(99)80028-X |
0.486 |
|
| 1998 |
Song O, Ju J, Librescu L. Dynamic Response Of Anisotropic Thin-Walled Beams To Blast And Harmonically Oscillating Loads International Journal of Impact Engineering. 21: 663-682. DOI: 10.1016/S0734-743X(98)00019-0 |
0.481 |
|
| 1998 |
Hause T, Librescu L, Camarda CJ. Postbuckling of anisotropic flat and doubly-curved sandwich panels under complex loading conditions International Journal of Solids and Structures. 35: 3007-3027. DOI: 10.1016/S0020-7683(97)00360-0 |
0.385 |
|
| 1998 |
Hause T, Librescu L, Johnson TF. Non-linear response of geometrically imperfect sandwich curved panels under thermomechanical loading International Journal of Non-Linear Mechanics. 33: 1039-1059. DOI: 10.1016/S0020-7462(97)00067-X |
0.405 |
|
| 1998 |
Lin W, Librescu L. Thermomechanical Postbuckling Of Geometrically Imperfect Shear–Deformable Flat And Curved Panels On A Nonlinear Elastic Foundation International Journal of Engineering Science. 36: 189-206. DOI: 10.1016/S0020-7225(97)00055-4 |
0.436 |
|
| 1997 |
Librescu L, Meirovitch L, Na SS. Control of cantilever vibration via structural tailoring and adaptive materials Aiaa Journal. 35: 1309-1315. DOI: 10.2514/2.262 |
0.412 |
|
| 1997 |
Librescu L, Hause T, Camarda CJ. Geometrically Nonlinear Theory of Initially Imperfect Sandwich Curved Panels Incorporating Nonclassical Effects Aiaa Journal. 35: 1393-1403. DOI: 10.2514/2.249 |
0.436 |
|
| 1997 |
Librescu L, Na SS. Vibration and dynamic response control of cantilevers carrying externally mounted stores Journal of the Acoustical Society of America. 102: 3516-3522. DOI: 10.1121/1.420397 |
0.472 |
|
| 1997 |
Sciuva MD, Icardi U, Librescu L. On modeling of laminated composite structures featuring interlaminae imperfections Studies in Applied Mechanics. 45: 395-404. DOI: 10.1016/S0922-5382(97)80041-4 |
0.464 |
|
| 1997 |
Librescu L, Lin W. Vibration of thermomechanically loaded flat and curved panels taking into account geometric imperfections and tangential edge restraints International Journal of Solids and Structures. 34: 2161-2181. DOI: 10.1016/S0020-7683(96)00025-X |
0.438 |
|
| 1997 |
Librescu L, Lin W. Postbuckling and vibration of shear deformable flat and curved panels on a non-linear elastic foundation International Journal of Non-Linear Mechanics. 32: 211-225. DOI: 10.1016/S0020-7462(96)00057-1 |
0.466 |
|
| 1997 |
Song O, Librescu L. Anisotropy And Structural Coupling On Vibration And Instability Of Spinning Thin-Walled Beams Journal of Sound and Vibration. 204: 477-494. DOI: 10.1006/Jsvi.1996.0947 |
0.435 |
|
| 1996 |
Librescu L, Meirovitch L, Song O. Integrated structural tailoring and control using adaptive materials for advanced aircraft wings Journal of Aircraft. 33: 203-213. DOI: 10.2514/3.46923 |
0.415 |
|
| 1996 |
Karpouzian G, Librescu L. Nonclassical effects on divergence and flutter of anisotropic swept aircraft wings Aiaa Journal. 34: 786-794. DOI: 10.2514/3.13141 |
0.402 |
|
| 1996 |
Song O, Librescu L. Bending vibrations of adaptive cantilevers with external stores International Journal of Mechanical Sciences. 38: 483-498. DOI: 10.1016/0020-7403(95)00075-5 |
0.442 |
|
| 1995 |
Song OS, Librescu L. Bending Vibration Of Cantilevered Thin-Walled Beams Subjected To Time-Dependent External Excitations Journal of the Acoustical Society of America. 98: 313-319. DOI: 10.1121/1.414358 |
0.426 |
|
| 1995 |
Bhaskar K, Librescu L. Buckling under axial compression of thin-walled composite beams exhibiting extension-twist coupling Composite Structures. 31: 203-212. DOI: 10.1016/0263-8223(95)00010-0 |
0.431 |
|
| 1995 |
Chang M-, Librescu L. Postbuckling of shear-deformable flat and curved panels under combined loading conditions International Journal of Mechanical Sciences. 37: 121-143. DOI: 10.1016/0020-7403(94)E0000-9 |
0.413 |
|
| 1995 |
Bhaskar K, Librescu L. A geometrically non-linear theory for laminated anisotropic thin-walled beams International Journal of Engineering Science. 33: 1331-1344. DOI: 10.1016/0020-7225(94)00118-4 |
0.445 |
|
| 1995 |
Librescu L, Reddy JN. Comments and authors' reply on “On vibration and buckling of symmetric laminated plates according to shear deformation theories. Part I and II”, by A. Nosier and J. N. Reddy Acta Mechanica. 110: 241-244. DOI: 10.1007/Bf01215427 |
0.376 |
|
| 1994 |
Karpouzian G, Librescu L. Comprehensive Model of Anisotropic Composite Aircraft Wings Suitable for Aeroelastic Analyses Journal of Aircraft. 31: 703-712. DOI: 10.2514/3.46551 |
0.505 |
|
| 1994 |
Song O, Librescu L, Rogers CA. Adaptive Response Control of Cantilevered Thin-Walled Beams Carrying Heavy Concentrated Masses Journal of Intelligent Material Systems and Structures. 5: 42-48. DOI: 10.1177/1045389X9400500105 |
0.377 |
|
| 1994 |
Schmidt R, Librescu L. Further results concerning the refined theory of anisotropic laminated composite plates Journal of Engineering Mathematics. 28: 407-425. DOI: 10.1007/Bf00058463 |
0.442 |
|
| 1993 |
Librescu L, Souza MA. Post-buckling of geometrically imperfect shear-deformable flat panels under combined thermal and compressive edge loadings Journal of Applied Mechanics. 60: 526-533. DOI: 10.1115/1.2900825 |
0.453 |
|
| 1993 |
Librescu L, Song O, Rogers CA. Adaptive vibrational behavior of cantilevered structures modeled as composite thin-walled beams International Journal of Engineering Science. 31: 775-792. DOI: 10.1016/0020-7225(93)90123-C |
0.46 |
|
| 1993 |
Librescu L, Chang MY. Effects of geometric imperfections on vibration of compressed shear deformable laminated composite curved panels Acta Mechanica. 96: 203-224. DOI: 10.1007/Bf01340710 |
0.467 |
|
| 1993 |
Song O, Librescu L. Free Vibration Of Anisotropic Composite Thin-Walled Beams Of Closed Cross-Section Contour Journal of Sound and Vibration. 167: 129-147. DOI: 10.1006/Jsvi.1993.1325 |
0.464 |
|
| 1992 |
Song O, Librescu L, Rogers CA. Application of adaptive technology to static aeroelastic control of wing structures Aiaa Journal. 30: 2882-2889. DOI: 10.2514/3.11633 |
0.412 |
|
| 1992 |
Librescu L, Chang MY. Vibration of compressively loaded shear deformable flat panels exhibiting initial geometric imperfections Aiaa Journal. 30: 2793-2795. DOI: 10.2514/3.11305 |
0.409 |
|
| 1992 |
Librescu L, Song O. On the static aeroelastic tailoring of composite aircraft swept wings modelled as thin-walled beam structures☆ Composites Engineering. 2: 497-512. DOI: 10.1016/0961-9526(92)90039-9 |
0.469 |
|
| 1992 |
Librescu L, Chang M-. Imperfection sensitivity and postbuckling behavior of shear-deformable composite doubly-curved shallow panels International Journal of Solids and Structures. 29: 1065-1083. DOI: 10.1016/0020-7683(92)90136-H |
0.429 |
|
| 1991 |
Librescu L, Thangjitham S. Analytical Studies on Static Aeroelastic Behavior of Forward-Swept Composite Wing Structures Journal of Aircraft. 28: 151-157. DOI: 10.2514/3.46004 |
0.42 |
|
| 1991 |
Librescu L, Song O. Behavior of Thin-Walled Beams Made of Advanced Composite Materials and Incorporating Non-Classical Effects Applied Mechanics Reviews. 44. DOI: 10.1115/1.3121352 |
0.438 |
|
| 1991 |
Librescu L, Stein M. A geometrically nonlinear theory of transversely isotropic laminated composite plates and its use in the post-buckling analysis Thin-Walled Structures. 11: 177-201. DOI: 10.1016/0263-8231(91)90016-C |
0.448 |
|
| 1991 |
Librescu L. Formulation Of An Elastodynamic Theory Of Laminated Shear-Deformable Flat Panels Journal of Sound and Vibration. 147: 1-12. DOI: 10.1016/0022-460X(91)90680-I |
0.395 |
|
| 1991 |
Librescu L, Schmidt R. Substantiation of a shear-deformable theory of anisotropic composite laminated shells accounting for the interlaminae continuity conditions International Journal of Engineering Science. 29: 669-683. DOI: 10.1016/0020-7225(91)90097-M |
0.423 |
|
| 1990 |
Librescu L, Stein M. Postbuckling of Shear Deformable Composite Flat Panels Taking Into Account Geometrical Imperfections Aiaa Journal. 30: 1352-1360. DOI: 10.2514/3.11071 |
0.457 |
|
| 1990 |
Librescu L, Nosier A. Response of laminated composite flat panels to sonic boom and explosive blast loadings Aiaa Journal. 28: 345-352. DOI: 10.2514/3.10395 |
0.464 |
|
| 1990 |
Nosier A, Librescu L, Frederick D. The effects of time-dependent excitation on the oscillatory motion of viscously damped laminated composite flat panels Studies in Applied Mechanics. 24: 249-268. DOI: 10.1016/B978-0-444-88366-7.50016-6 |
0.484 |
|
| 1990 |
Stein M, Sydow PD, Librescu L. Postbuckling of Long Thick Plates in Compression Including Higher Order Transverse Shearing Effects Studies in Applied Mechanics. 24: 63-86. DOI: 10.1016/B978-0-444-88366-7.50008-7 |
0.418 |
|
| 1990 |
Cederbaum G, Elishakoff I, Librescu L. Reliability of laminated plates via the first-order second-moment method Composite Structures. 15: 161-167. DOI: 10.1016/0263-8223(90)90005-Y |
0.327 |
|
| 1990 |
Birman V, Librescu L. Supersonic flutter of shear deformable laminated composite flat panels Journal of Sound and Vibration. 139: 265-275. DOI: 10.1016/0022-460X(90)90887-6 |
0.428 |
|
| 1990 |
Librescu L, Thangjitham S. Parametric instability of laminated composite shear-deformable flat panels subjected to in-plane edge loads International Journal of Non-Linear Mechanics. 25: 263-273. DOI: 10.1016/0020-7462(90)90056-F |
0.461 |
|
| 1990 |
Librescu L, Khdeir AA, Reddy JN. Further Results Concerning the Dynamic Response of Shear Deformable Elastic Orthotropic Plates Zamm-Zeitschrift Fur Angewandte Mathematik Und Mechanik. 70: 23-33. DOI: 10.1002/Zamm.19900700108 |
0.451 |
|
| 1989 |
Elishakoff I, Cederbaum G, Librescu L. Response of moderately thick laminated cross-ply composite shells subjected to random excitation Aiaa Journal. 27: 975-981. DOI: 10.2514/3.10207 |
0.442 |
|
| 1989 |
Chandiramani NK, Librescu L. Dynamic Stability of Unidirectional Fiber-Reinforced Viscoelastic Composite Plates Applied Mechanics Reviews. 42. DOI: 10.1115/1.3152405 |
0.456 |
|
| 1989 |
Cederbaum G, Elishakoff I, Librescu L. Random vibrations of laminated plates modeled within the first order shear deformation theory Composite Structures. 12: 97-111. DOI: 10.1016/0263-8223(89)90084-6 |
0.455 |
|
| 1989 |
Cederbaum G, Librescu L, Elishakoff I. Response of laminated plates to non-stationary random excitation Structural Safety. 6: 99-113. DOI: 10.1016/0167-4730(89)90013-1 |
0.385 |
|
| 1989 |
Librescu L, Chandiramani NK. Dynamic stability of transversely isotropic viscoelastic plates Journal of Sound and Vibration. 130: 467-486. DOI: 10.1016/0022-460X(89)90070-9 |
0.451 |
|
| 1989 |
Cederbaum G, Librescu L, Elishakoff I. Remarks on a dynamical higher-order theory of laminated plates and its application in random vibration response International Journal of Solids and Structures. 25: 515-526. DOI: 10.1016/0020-7683(89)90063-2 |
0.407 |
|
| 1989 |
Chandiramani NK, Librescu L, Aboudi J. The theory of orthotropic viscoelastic shear deformable composite flat panels and their dynamic stability International Journal of Solids and Structures. 25: 465-482. DOI: 10.1016/0020-7683(89)90060-7 |
0.446 |
|
| 1989 |
Librescu L, Reddy JN. A few remarks concerning several refined theories of anisotropic composite laminated plates International Journal of Engineering Science. 27: 515-527. DOI: 10.1016/0020-7225(89)90004-9 |
0.388 |
|
| 1989 |
Khdeir AA, Librescu L, Frederick D. A shear deformable theory of laminated composite shallow shell-type panels and their response analysis. II - Static response Acta Mechanica. 77: 1-12. DOI: 10.1007/Bf01379740 |
0.44 |
|
| 1989 |
Librescu L, Khdeir AA, Frederick D. A shear deformable theory of laminated composite shallow shell-type panels and their response analysis I: Free vibration and buckling Acta Mechanica. 76: 1-33. DOI: 10.1007/Bf01175794 |
0.431 |
|
| 1988 |
Librescu L, Simovich J. General formulation for the aeroelastic divergence of composite swept-forward wing structures Journal of Aircraft. 25: 364-371. DOI: 10.2514/3.45572 |
0.382 |
|
| 1988 |
Librescu L, Khdeir AA. Aeroelastic divergence of swept-forward composite wings including warping restraint effect Aiaa Journal. 26: 1373-1377. DOI: 10.2514/3.10050 |
0.371 |
|
| 1988 |
Cederbaum G, Librescu L, Elishakoff I. Random vibration of laminated plates modeled within a high‐order shear deformation theory Journal of the Acoustical Society of America. 84: 660-666. DOI: 10.1121/1.396845 |
0.436 |
|
| 1988 |
Khdeir AA, Librescu L. Analysis of symmetric cross-ply laminated elastic plates using a higher-order theory. II - Buckling and free vibration Composite Structures. 9: 259-277. DOI: 10.1016/0263-8223(88)90048-7 |
0.414 |
|
| 1988 |
Librescu L, Khdeir AA. Analysis of symmetric cross ply laminated elastic plates using a higher-order theory. I: Stress and displacement Composite Structures. 9: 189-213. DOI: 10.1016/0263-8223(88)90014-1 |
0.404 |
|
| 1987 |
Reddy JN, Khdeir AA, Librescu L. Lévy Type Solutions for Symmetrically Laminated Rectangular Plates Using First-Order Shear Deformation Theory Journal of Applied Mechanics. 54: 740-742. DOI: 10.1115/1.3173104 |
0.361 |
|
| 1987 |
Khdeir AA, Reddy JN, Librescu L. Analytical solution of a refined shear deformation theory for rectangular composite plates International Journal of Solids and Structures. 23: 1447-1463. DOI: 10.1016/0020-7683(87)90009-6 |
0.409 |
|
| 1987 |
Librescu L, Khdeir AA, Reddy JN. A comprehensive analysis of the state of stress of elastic anisotropic flat plates using refined theories Acta Mechanica. 70: 57-81. DOI: 10.1007/Bf01174647 |
0.367 |
|
| 1967 |
Librescu L. On the theory of anisotropic elastic shells and plates International Journal of Solids and Structures. 3: 53-68. DOI: 10.1016/0020-7683(67)90044-3 |
0.428 |
|
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