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Mayuresh J. Patil - Publications

Affiliations: 
Aerospace Engineering Virginia Polytechnic Institute and State University, Blacksburg, VA, United States 
Area:
Aerospace Engineering
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55 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 Sharma H, Patil M, Woolsey C. A review of structure-preserving numerical methods for engineering applications Computer Methods in Applied Mechanics and Engineering. 366: 113067. DOI: 10.1016/J.Cma.2020.113067  0.319
2018 Sharma H, Patil M, Woolsey C. Energy-preserving variational integrators for forced Lagrangian systems Communications in Nonlinear Science and Numerical Simulation. 64: 159-177. DOI: 10.1016/J.Cnsns.2018.04.015  0.329
2017 Shukla H, Patil MJ. Controlling Limit Cycle Oscillation Amplitudes in Nonlinear Aeroelastic Systems Journal of Aircraft. 54: 1921-1932. DOI: 10.2514/1.C034239  0.608
2017 Shukla H, Patil MJ. Nonlinear state feedback control design to eliminate subcritical limit cycle oscillations in aeroelastic systems Nonlinear Dynamics. 88: 1599-1614. DOI: 10.1007/S11071-017-3332-5  0.473
2016 Stewart EC, Patil MJ, Canfield RA, Snyder RD. Aeroelastic shape optimization of a flapping wing Journal of Aircraft. 53: 636-650. DOI: 10.2514/1.C033278  0.34
2016 Ricciardi AP, Canfield RA, Patil MJ, Lindsley N. Nonlinear aeroelastic scaled-model design Journal of Aircraft. 53: 20-32. DOI: 10.2514/1.C033171  0.369
2016 Shukla H, Patil MJ. Control of limit cycle oscillation amplitudes in nonlinear aeroelastic systems using nonlinear normal modes Aiaa Atmospheric Flight Mechanics Conference.  0.505
2014 Ricciardi AP, Eger CAG, Canfield RA, Patil MJ. Nonlinear aeroelastic-scaled-model optimization using equivalent static loads Journal of Aircraft. 51: 1842-1851. DOI: 10.2514/1.C032539  0.484
2014 Bhatia M, Patil M, Woolsey C, Stanford B, Beran P. Stabilization of flapping-wing micro-air vehicles in gust environments Journal of Guidance, Control, and Dynamics. 37: 592-607. DOI: 10.2514/1.59875  0.467
2013 Ricciardi AP, Eger CAG, Canfield RA, Patil MJ. Nonlinear aeroelastic scaled model optimization using equivalent static loads Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference. DOI: 10.2514/6.2013-1785  0.304
2013 Ricciardi AP, Patil MJ, Canfield RA, Lindsley N. Evaluation of quasi-static gust loads certification methods for high-altitude long-endurance aircraft Journal of Aircraft. 50: 457-468. DOI: 10.2514/1.C031872  0.389
2013 Emory CW, Patil MJ. Predicting limit cycle oscillation in an aeroelastic system using nonlinear normal modes Journal of Aircraft. 50: 73-81. DOI: 10.2514/1.C031668  0.649
2013 Stanford B, Beran P, Patil M. Optimal Flapping-Wing Vehicle Dynamics via Floquet Multiplier Sensitivities Journal of Guidance Control and Dynamics. 36: 454-466. DOI: 10.2514/1.57213  0.391
2013 Stanford B, Beran P, Snyder R, Patil M. Stability and power optimality in time-periodic flapping wing structures Journal of Fluids and Structures. 38: 238-254. DOI: 10.1016/J.Jfluidstructs.2012.12.006  0.472
2013 Ricciardi AP, Eger CAG, Canfield RA, Patil MJ. Nonlinear aeroelastic scaled model optimization using equivalent static loads Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference.  0.429
2012 Althoff M, Patil MJ, Traugott JP. Nonlinear modeling and control design of active helicopter blades 012002 Journal of the American Helicopter Society. 57. DOI: 10.4050/Jahs.57.012002  0.456
2012 Ouellette JA, Patil MJ, Kapania RK. Scaling laws for flight control development and testing in the presence of aeroservoelastic interactions Aiaa Atmospheric Flight Mechanics Conference 2012. DOI: 10.2514/6.2012-4640  0.331
2012 Walker W, Patil M, Canfield R. Thrust and efficiency optimization of a harmonically deforming thin airfoil for MAV design International Journal of Micro Air Vehicles. 4: 93-117. DOI: 10.1260/1756-8293.4.2.93  0.309
2012 Ricciardi AP, Eger CAG, Canfield RA, Patil MJ, Lindsley N. High fidelity nonlinear aeroelastic analysis for scaled vehicle design 12th Aiaa Aviation Technology, Integration and Operations (Atio) Conference and 14th Aiaa/Issmo Multidisciplinary Analysis and Optimization Conference.  0.313
2012 Ricciardi AP, Canfield RA, Patil MJ, Lindsley N. Nonlinear aeroelastic scaling of a joined-wing aircraft 53rd Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference 2012.  0.409
2012 Ricciardi AP, Canfield RA, Patil MJ, Lindsley N. Nonlinear aeroelastic scaling of a joined-wing aircraft Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference.  0.356
2011 Emory CW, Patil MJ. Prediction of limit cycle oscillation in an aeroelastic system using asymptotic nonlinear normal modes Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference. DOI: 10.2514/6.2011-1742  0.657
2011 Patil MJ, Hodges DH. Variable-order finite elements for nonlinear, fully intrinsic beam equations Journal of Mechanics of Materials and Structures. 6: 479-493. DOI: 10.2140/Jomms.2011.6.479  0.373
2011 Patil MJ, Althoff M. Energy-consistent, Galerkin approach for the nonlinear dynamics of beams using intrinsic equations Jvc/Journal of Vibration and Control. 17: 1748-1758. DOI: 10.1177/1077546310385777  0.459
2011 Venturella MA, Patil MJ, McCue LS. Modal analysis of the ice-structure interaction problem Journal of Offshore Mechanics and Arctic Engineering. 133. DOI: 10.1115/1.4003388  0.335
2010 Walker WP, Patil MJ. Unsteady aerodynamics of deformable thin airfoils 48th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. DOI: 10.2514/1.C031434  0.317
2010 Raghavan B, Patil MJ. Flight control for flexible, high-aspect-ratio flying wings Journal of Guidance, Control, and Dynamics. 33: 64-74. DOI: 10.2514/1.45471  0.673
2010 Dang TD, Kapania RK, Patil MJ. Analytical modeling of cracked thin-walled beams under torsion Aiaa Journal. 48: 664-675. DOI: 10.2514/1.45393  0.306
2010 Richter MN, Patil MJ. Influence of wing flexibility on the stability of flapping flight Aiaa Atmospheric Flight Mechanics Conference 2010.  0.309
2009 Raghavan B, Patil MJ. Flight dynamics of high-aspect-ratio flying wings: Effect of large trim deformation Journal of Aircraft. 46: 1808-1812. DOI: 10.2514/1.36847  0.647
2009 Hodges DH, Yu W, Patil MJ. Geometrically-exact, intrinsic theory for dynamics of moving composite plates International Journal of Solids and Structures. 46: 2036-2042. DOI: 10.1016/J.Ijsolstr.2008.05.005  0.381
2009 Ouellette JA, Raghavan B, Patil MJ, Kapania RK. Flight dynamics and structural load distribution for a damaged aircraft Aiaa Atmospheric Flight Mechanics Conference.  0.595
2008 Chang CS, Hodges DH, Patil MJ. Flight dynamics of highly flexible aircraft Journal of Aircraft. 45: 538-545. DOI: 10.2514/1.30890  0.379
2008 Raghavan B, Patil MJ, Woolsey CA. Trajectory tracking for high aspect-ratio flying wings Aiaa Atmospheric Flight Mechanics Conference and Exhibit.  0.479
2007 Patil MJ. Nonlinear gust response of highly flexible aircraft Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference. 5: 4741-4753.  0.323
2006 Patil MJ, Hodges DH. Flight dynamics of highly flexible flying wings Journal of Aircraft. 43: 1790-1798. DOI: 10.2514/1.17640  0.527
2006 Traugott JP, Patil MJ, Holzapfel F. Nonlinear modeling of integrally actuated beams Aerospace Science and Technology. 10: 509-518. DOI: 10.1016/J.Ast.2006.06.003  0.438
2006 Wang Z, Chen PC, Liu DD, Mook DT, Patil MJ. Time domain nonlinear aeroelastic analysis for HALE wings Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference. 1: 488-506.  0.493
2005 Traugott JP, Patil MJ, Holzapfel F. Nonlinear dynamics and control of integrally actuated helicopter blades Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference. 9: 5847-5861.  0.344
2004 Patil MJ. Limit-cycle oscillations of aircraft caused by flutter-induced drag Journal of Aircraft. 41: 571-576. DOI: 10.2514/1.11482  0.408
2004 Patil MJ, Hodges DH. On the importance of aerodynamic and structural geometrical nonlinearities in aeroelastic behavior of high-aspect-ratio wings Journal of Fluids and Structures. 19: 905-915. DOI: 10.1016/J.Jfluidstructs.2004.04.012  0.514
2003 Patil MJ. Nonlinear aeroelastic analysis of joined-wing aircraft 44th Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics, and Materials Conference.  0.481
2003 Patil MJ. Nonlinear aeroelastic analysis of joined-wing aircraft 44th Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics, and Materials Conference.  0.481
2002 Patil MJ, Hodges DH. Output feedback control of the nonlinear aeroelastic response of a slender wing Journal of Guidance, Control, and Dynamics. 25: 302-308. DOI: 10.2514/2.4882  0.398
2002 Hodges DH, Patil MJ, Chae S. Effect of thrust on bending-torsion flutter of wings Journal of Aircraft. 39: 371-376. DOI: 10.2514/2.2937  0.406
2002 Patil MJ, Hodges DH, Cesnik CES. Limit-cycle oscillations in high-aspect-ratio wings Journal of Food Composition and Analysis. 15. DOI: 10.1006/Jfls.2000.0329  0.431
2002 Patil MJ. Limit cycle oscillations of aircraft due to flutter-induced drag Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference. 3: 1614-1624.  0.303
2001 Patil MJ. From fluttering wings to flapping flight: The energy connection 19th Aiaa Applied Aerodynamics Conference. DOI: 10.2514/2.3119  0.434
2001 Patil MJ, Hodges DH, Cesnik CES. Nonlinear aeroelasticity and flight dynamics of high-altitude long-endurance aircraft Journal of Aircraft. 38: 88-94. DOI: 10.2514/2.2738  0.457
2001 Patil MJ, Lee D, Hodges DH. Multi-flexible-body dynamic analysis of horizontal-axis wind turbines 20th 2001 Asme Wind Energy Symposium. DOI: 10.1002/We.66  0.401
2001 Lee D, Patil MJ, Hodges DH. A symbolic methodology for the stability analysis of flexible rotating systems Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference. 4: 2652-2661.  0.321
2001 Smith MJ, Patil MJ, Hodges DH. CFD-based analysis of nonlinear aeroelastic behavior of high-aspect ratio wings 19th Aiaa Applied Aerodynamics Conference.  0.408
2000 Patil MJ, Hodges DH, Cesnik CES. Nonlinear aeroelastic analysis of complete aircraft in subsonic flow Journal of Aircraft. 37: 753-760. DOI: 10.2514/2.2685  0.528
2000 Cesnik CES, Ortega-Morales M, Patil MJ. Active aeroelastic tailoring of high aspect ratio composite wings 41st Structures, Structural Dynamics, and Materials Conference and Exhibit.  0.363
1996 Cesnik CES, Hodges DH, Patil MJ. Aeroelastic analysis of composite wings 37th Aiaa/Asme/Asce/Ahs/Asc Structure, Structural Dynamics and Materials Conference. 1113-1123. DOI: 10.2514/6.1996-1444  0.309
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