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Farhan S. Gandhi - Publications

Affiliations: 
2012 Aerospace engineering Pennsylvania State University, State College, PA, United States 
 2012- Aerospace engineering Rensselaer Polytechnic Institute, Troy, NY, United States 
Area:
VTOL aircraft aeromechanics, advanced VTOL configurations, adaptive structures
Website:
https://move.rpi.edu/
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65 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 Misiorowski M, Gandhi F, Anusonti-Inthra P. Computational Analysis of Rotor-Blown-Wing for Electric Rotorcraft Applications Aiaa Journal. 58: 2921-2932. DOI: 10.2514/1.J058851  0.718
2018 Jacobellis G, Gandhi F, Floros M. Using Control Redundancy for Power and Vibration Reduction on a Coaxial Rotor Helicopter at High Speeds Journal of the American Helicopter Society. 63: 1-13. DOI: 10.4050/Jahs.63.032009  0.33
2018 Niemiec R, Gandhi F, Singh R. Control and Performance of a Reconfigurable Multicopter Journal of Aircraft. 55: 1855-1866. DOI: 10.2514/1.C034731  0.31
2014 Gandhi F, Duling C, Straub F. On power and actuation requirement in swashplateless primary control of helicopters using trailing-edge flaps Aeronautical Journal. 118: 503-521. DOI: 10.1017/S0001924000009337  0.381
2013 Pontecorvo ME, Barbarino S, Murray GJ, Gandhi FS. Bistable arches for morphing applications Journal of Intelligent Material Systems and Structures. 24: 274-286. DOI: 10.1177/1045389X12457252  0.638
2013 Miller TF, Gandhi F, Rufino RJ. Morphing hull implementation for unmanned underwater vehicles Smart Materials and Structures. 22. DOI: 10.1088/0964-1726/22/11/115014  0.362
2013 Atli-Veltin B, Gandhi F. Energy absorption of sandwiched honeycombs with facesheets under in-plane crushing Aeronautical Journal. 117: 687-708. DOI: 10.1017/S000192400000837X  0.75
2012 Austruy J, Gandhi F, Lieven N. Rotor vibration reduction using an embedded spanwise absorber Journal of the American Helicopter Society. 57. DOI: 10.4050/Jahs.57.022008  0.792
2012 Murray G, Gandhi F, Hayden E. Polymer-filled honeycombs to achieve a structural material with appreciable damping Journal of Intelligent Material Systems and Structures. 23: 703-718. DOI: 10.1177/1045389X12439636  0.614
2012 Olympio KR, Gandhi F. Optimal cellular core topologies for one-dimensional morphing aircraft structures Journal of Mechanical Design, Transactions of the Asme. 134. DOI: 10.1115/1.4007087  0.783
2012 Raither W, Bergamini A, Gandhi F, Ermanni P. Adaptive bending-twist coupling in laminated composite plates by controllable shear stress transfer Composites Part a-Applied Science and Manufacturing. 43: 1709-1716. DOI: 10.1016/J.Compositesa.2012.01.015  0.32
2011 Bluman JE, Gandhi FS. Reducing trailing edge flap deflection requirements in primary control with a movable horizontal tail Journal of the American Helicopter Society. 56. DOI: 10.4050/Jahs.56.032005  0.353
2011 Barbarino S, Gandhi F, Webster SD. Design of Extendable Chord Sections for Morphing Helicopter Rotor Blades Journal of Intelligent Material Systems and Structures. 22: 891-905. DOI: 10.1177/1045389X11414077  0.336
2010 Kang H, Saberi H, Gandhi F. Dynamic Blade Shape for Improved Helicopter Rotor Performance Journal of the American Helicopter Society. 55: 32008-3200811. DOI: 10.4050/Jahs.55.032008  0.326
2010 Malovrh B, Gandhi F. Localized Individual Blade Root Pitch Control for Helicopter Blade—Vortex Interaction Noise Reduction Journal of the American Helicopter Society. 55: 32007-3200712. DOI: 10.4050/Jahs.55.032007  0.77
2010 Atli-Veltin B, Gandhi F. Effect of cell geometry on energy absorption of honeycombs under in-plane compression Aiaa Journal. 48: 466-478. DOI: 10.2514/1.45021  0.767
2010 Paik J, Gandhi F. Design optimization for improved soft in-plane tiltrotor aeroelastic stability in airplane mode Journal of Aircraft. 47: 1089-1099. DOI: 10.2514/1.43212  0.646
2010 Murray GJ, Gandhi F. Auxetic honeycombs with lossy polymeric infills for high damping structural materials 21st International Conference On Adaptive Structures and Technologies 2010, Icast 2010. 96-105. DOI: 10.1177/1045389X13480569  0.615
2010 Olympio KR, Gandhi F, Asheghian L, Kudva J. Design of a flexible skin for a shear morphing wing Journal of Intelligent Material Systems and Structures. 21: 1755-1770. DOI: 10.1177/1045389X10382586  0.782
2010 Murray G, Gandhi F, Bakis C. Flexible Matrix Composite Skins for One-dimensional Wing Morphing Journal of Intelligent Material Systems and Structures. 21: 1771-1781. DOI: 10.1177/1045389X10369719  0.613
2010 Olympio KR, Gandhi F. Zero poisson's ratio cellular honeycombs for flex skins undergoing one-dimensional morphing Journal of Intelligent Material Systems and Structures. 21: 1737-1753. DOI: 10.1177/1045389X09355664  0.787
2010 Olympio KR, Gandhi F. Flexible skins for morphing aircraft using cellular honeycomb cores Journal of Intelligent Material Systems and Structures. 21: 1719-1735. DOI: 10.1177/1045389X09350331  0.775
2010 Johnson T, Gandhi F, Frecker M. Modeling and experimental validation of a bistable mechanism for chord extension morphing Proceedings of Spie - the International Society For Optical Engineering. 7643. DOI: 10.1117/12.847661  0.319
2009 Johnson T, Frecker M, Gandhi F. A bistable mechanism for chord extension morphing rotors Proceedings of Spie - the International Society For Optical Engineering. 7288. DOI: 10.1117/12.815472  0.425
2009 Byers L, Gandhi F. Embedded absorbers for helicopter rotor lag damping Journal of Sound and Vibration. 325: 705-721. DOI: 10.1016/J.Jsv.2009.03.031  0.803
2008 Gandhi F, Frecker M, Nissly A. Design optimization of a controllable camber rotor airfoil Aiaa Journal. 46: 142-153. DOI: 10.2514/1.24476  0.417
2008 Mehta V, Brennan S, Gandhi F. Experimentally Verified Optimal Serpentine Gait and Hyperredundancy of a Rigid-Link Snake Robot Ieee Transactions On Robotics. 24: 348-360. DOI: 10.1109/Tro.2008.915441  0.338
2008 Gandhi F, Anusonti-Inthra P. Skin design studies for variable camber morphing airfoils Smart Materials and Structures. 17. DOI: 10.1088/0964-1726/17/01/015025  0.734
2007 Hathaway EL, Gandhi F. Design optimization for improved tiltrotor whirl flutter stability Journal of the American Helicopter Society. 52: 79-89. DOI: 10.4050/Jahs.52.79  0.779
2007 Paik J, Singh R, Gandhi F, Hathaway E. Active Tiltrotor Whirl-Flutter Stability Augmentation Using Wing-Flaperon and Swash-plate Actuation Journal of Aircraft. 44: 1439-1446. DOI: 10.2514/1.20234  0.779
2007 Gandhi F, Remillat C, Tomlinson G, Austruy J. Constrained-layer damping with gradient polymers for effectiveness over broad temperature ranges Aiaa Journal. 45: 1885-1893. DOI: 10.2514/1.19574  0.751
2006 Hathaway EL, Gandhi F. Tiltrotor whirl flutter alleviation using actively controlled wing flaperons Aiaa Journal. 44: 2524-2534. DOI: 10.2514/1.18428  0.784
2006 Malovrh B, Gandhi F. Partial Hyperbolic-Tangent Friction Element Based Phenomenological Models for Shape Memory Alloy Pseudoelastic Hysteresis Journal of Engineering Materials and Technology-Transactions of the Asme. 128: 346-355. DOI: 10.1115/1.2204941  0.769
2005 Malovrh B, Gandhi F. Sensitivity of helicopter blade-vortex-interaction noise and vibration to interaction parameters Journal of Aircraft. 42: 685-697. DOI: 10.2514/1.4466  0.793
2005 Anusonti-Inthra P, Sarjeant R, Frecker M, Gandhi F. Design of a Comfortable Rotor Airfoil Using Distributed Piezoelectric Actuators Aiaa Journal. 43: 1684-1695. DOI: 10.2514/1.1519  0.756
2004 Gandhi F, Sekula MK. Helicopter Vibration Reduction Using Fixed-System Auxiliary Moments Aiaa Journal. 42: 501-512. DOI: 10.2514/1.575  0.76
2004 Sekula MK, Gandhi F. Effects of Auxiliary Lift and Propulsion on Helicopter Vibration Reduction and Trim Journal of Aircraft. 41: 645-656. DOI: 10.2514/1.496  0.762
2004 Marathe SS, Wang KW, Gandhi F. Feedback linearization control of magnetorheological fluid damper based systems with model uncertainty Smart Materials and Structures. 13: 1006-1016. DOI: 10.1088/0964-1726/13/5/005  0.345
2004 Anusonti-Inthra P, Gandhi F. Cyclic modulation of semi-active controllable dampers for tonal vibration isolation Journal of Sound and Vibration. 275: 107-126. DOI: 10.1016/S0022-460X(03)00788-0  0.745
2003 Gandhi F, Tauszig L. A Method to Evaluate the Contributions of Individual Interactions to Helicopter Blade-Vortex Interaction Noise Journal of the American Helicopter Society. 48: 287-299. DOI: 10.4050/Jahs.48.287  0.748
2003 Hathaway EL, Gandhi FS. Modeling refinements in simple tiltrotor whirl flutter analyses Journal of the American Helicopter Society. 48: 186-198. DOI: 10.4050/Jahs.48.186  0.748
2003 Gandhi F, Anusonti-Inthra P. Adaptive control of semiactive variable stiffness devices for narrow-band disturbance rejection Journal of Intelligent Material Systems and Structures. 14: 191-201. DOI: 10.1177/1045389X03014003007  0.739
2003 Anusonti-Inthra P, Gandhi F, Miller L. Reduction of helicopter vibration through cyclic control of variable orifice dampers Aeronautical Journal. 107: 657-672. DOI: 10.1017/S0001924000013531  0.772
2002 Gandhi F, Munsky B. Effectiveness of Active Constrained Layer Damping Treatments in Attenuating Resonant Oscillations Journal of Vibration and Control. 8: 747-775. DOI: 10.1177/1077546029188  0.358
2002 Gandhi F, Munsky B. Comparison of Damping Augmentation Mechanisms with Position and Velocity Feedback in Active Constrained Layer Treatments Journal of Intelligent Material Systems and Structures. 13: 317-326. DOI: 10.1177/104538902761696788  0.351
2002 Gandhi F, Chapuis G. Passive damping augmentation of a vibrating beam using pseudoelastic shape memory alloy wires Journal of Sound and Vibration. 250: 519-539. DOI: 10.1006/Jsvi.2001.3935  0.376
2001 Gandhi F, Anusonti-Inthra P. Helicopter Vibration Reduction Using Discrete Controllable-Stiffness Devices at the Rotor Hub Journal of Aircraft. 39: 668-677. DOI: 10.2514/2.2980  0.745
2001 Hathaway E, Gandhi F. Concurrently Optimized Aeroelastic Couplings and Rotor Stiffness for Alleviation of Helicopter Aeromechanical Instability Journal of Aircraft. 38: 69-80. DOI: 10.2514/2.2736  0.79
2001 Gandhi F. Influence of Nonlinear Viscoelastic Material Characterization on Performance of Constrained Layer Damping Treatment Aiaa Journal. 39: 924-931. DOI: 10.2514/2.1397  0.318
2001 Malovrh B, Gandhi F. Mechanism-Based Phenomenological Models for the Pseudoelastic Hysteresis Behavior of Shape Memory Alloys Journal of Intelligent Material Systems and Structures. 12: 21-30. DOI: 10.1106/Xf8T-Pfkl-4Kjk-6V6H  0.776
2001 Gandhi F, Wang KW, Xia L. Magnetorheological fluid damper feedback linearization control for helicopter rotor application Smart Materials and Structures. 10: 96-103. DOI: 10.1088/0964-1726/10/1/309  0.356
2001 Anusonti-Inthra P, Gandhi F. Optimal control of helicopter vibration through cyclic variations in blade root stiffness Smart Materials and Structures. 10: 86-95. DOI: 10.1088/0964-1726/10/1/308  0.767
2001 Tauszig L, Gandhi F. Influence of blade-to-blade dissimilarity on alleviation of helicopter blade-vortex interactions Mathematical and Computer Modelling. 33: 1139-1154. DOI: 10.1016/S0895-7177(00)00304-6  0.78
2000 Gandhi F, Tauszig L. A Critical Evaluation of Various Approaches for the Numerical Detection of Helicopter Blade-Vortex Interactions Journal of the American Helicopter Society. 45: 179. DOI: 10.4050/Jahs.45.179  0.745
2000 Anusonti-Inthra P, Gandhi F. Helicopter vibration reduction through cyclic variations in rotor blade root stiffness Journal of Intelligent Material Systems and Structures. 11: 153-166. DOI: 10.1106/B8Nq-4Lnn-Mppl-Afhv  0.761
1999 Gandhi F, Malovrh B. Influence of balanced rotor anisotropy on helicopter aeromechanical stability Aiaa Journal. 37: 1152-1160. DOI: 10.2514/2.600  0.794
1999 Badre-Alam A, Wang KW, Gandhi F. Optimization of enhanced active constrained layer (EACL) treatment on helicopter flexbeams for aeromechanical stability augmentation Smart Materials and Structures. 8: 182-196. DOI: 10.1088/0964-1726/8/2/003  0.379
1999 Gandhi F, Wolons D. Characterization of the pseudoelastic damping behavior of shape memory alloy wires using complex modulus Smart Materials and Structures. 8: 49-56. DOI: 10.1088/0964-1726/8/1/005  0.341
1998 Gandhi F, Chopra I. An Aeroelastic Analysis Methodology for Bearingless Main Rotor Helicopters Journal of the American Helicopter Society. 43: 66-75. DOI: 10.4050/Jahs.43.66  0.517
1998 Gandhi F, Hathaway E. Optimized Aeroelastic Couplings for Alleviation of Helicopter Ground Resonance Journal of Aircraft. 35: 582-590. DOI: 10.2514/2.2341  0.783
1998 Marathe S, Gandhi F, Wang KW. Helicopter Blade Response and Aeromechanical Stability with a Magnetorheological Fluid Based Lag Damper Journal of Intelligent Material Systems and Structures. 9: 272-282. DOI: 10.1177/1045389X9800900405  0.313
1998 Wolons D, Gandhi F, Malovrh B. Experimental Investigation of the Pseudoelastic Hysteresis Damping Characteristics of Shape Memory Alloy Wires Journal of Intelligent Material Systems and Structures. 9: 116-126. DOI: 10.1177/1045389X9800900205  0.774
1996 Gandhi F, Chopra I. Analysis of Bearingless Main Rotor Aeroelasticity Using an Improved Time Domain Nonlinear Elastomeric Damper Model Journal of the American Helicopter Society. 41: 267-277. DOI: 10.4050/Jahs.41.267  0.499
1996 Gandhi F, Chopra I. A time-domain non-linear viscoelastic damper model Smart Materials and Structures. 5: 517-528. DOI: 10.1088/0964-1726/5/5/002  0.526
1994 Gandhi F, Chopra I. An Analytical Model for a Nonlinear Elastomeric Lag Damper and Its Effect on Aeromechanical Stability in Hover Journal of the American Helicopter Society. 39: 59-69. DOI: 10.4050/Jahs.39.59  0.499
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