| Survey and comparison of engineering beam theories for helicopter rotor blades DL Kunz Journal of Aircraft 31 (3), 473-479, 1994 | 74 | 1994 |
| Influence of elastomeric damper modeling on the dynamic response of helicopter rotors DL Kunz AIAA journal 35 (2), 349-354, 1997 | 54 | 1997 |
| A comparison of main rotor smoothing adjustments using linear and neural network algorithms NA Miller, DL Kunz Journal of Sound and Vibration 311 (3-5), 991-1003, 2008 | 47 | 2008 |
| Comprehensive rotorcraft analysis: Past, present, and future D Kunz 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials …, 2005 | 41 | 2005 |
| Dynamic coupling of the KC-135 tanker and boom for modeling and simulation AL Smith, DL Kunz Journal of aircraft 44 (3), 1034-1039, 2007 | 38 | 2007 |
| Introduction to GRASP—General Rotorcraft Aeromechanical Stability Program—A Modern Approach to Rotorcraft Modeling DH Hodges, AS Hopkins, DL Kunz, HE Hinnant Journal of the American Helicopter Society 32 (2), 78-90, 1987 | 38 | 1987 |
| The effect of varying freestream velocity on airfoil dynamic stall characteristics GA Pierce, DL Kunz, JB Malone Journal of the American Helicopter Society 23 (2), 27-33, 1978 | 34 | 1978 |
| Analysis of proprotor whirl flutter: review and update DL Kunz Journal of aircraft 42 (1), 172-178, 2005 | 33 | 2005 |
| Nonlinear analysis of helicopter ground resonance DL Kunz Nonlinear Analysis: real world applications 3 (3), 383-395, 2002 | 30 | 2002 |
| Numerical simulations of cantilever beam response with saturation control and full modal coupling S Saguranrum, DL Kunz, HM Omar Computers & structures 81 (14), 1499-1510, 2003 | 26 | 2003 |
| An object-oriented approach to multibody systems analysis DL Kunz Computers & structures 69 (2), 209-217, 1998 | 26 | 1998 |
| Alleviation of buffet-induced vibration using piezoelectric actuators RA Canfield, SD Morgenstern, DL Kunz Computers & structures 86 (3-5), 281-291, 2008 | 25 | 2008 |
| Analysis of structures with rotating, flexible substructures appliedto rotorcraft aeroelasticity DH Hodges, AS Hopkins, DL Kunz AIAA journal 27 (2), 192-200, 1989 | 19 | 1989 |
| A generalized dynamic balancing procedure for the AH-64 tail rotor DL Kunz, MC Newkirk Journal of Sound and Vibration 326 (1-2), 353-366, 2009 | 17 | 2009 |
| Experiments with geometric nonlinear coupling for analytical validation J Boston, E Swenson, D Kunz, W Yu, M Blair Journal of Aircraft 48 (4), 1136-1146, 2011 | 14 | 2011 |
| Elastomer modelling for use in predicting helicopter lag damper behavior DL Kunz Journal of sound and vibration 226 (3), 585-594, 1999 | 12 | 1999 |
| Toward a Flying Qualities Standard for Unmanned Aircraft KM Greene, DL Kunz, MC Cotting AIAA Atmospheric Flight Mechanics Conference, 2194, 2014 | 11 | 2014 |
| Multibody system analysis based on Hamilton's weak principle DL Kunz AIAA journal 39 (12), 2382-2388, 2001 | 11 | 2001 |
| A nonlinear response analysis and solution method for rotorcraft vibration DL Kunz Journal of the American Helicopter Society 28 (1), 56-62, 1983 | 10 | 1983 |
| Maximal Distance Discounted and Weighted Revisit Period: A Utility Approach to Persistent Unmanned Surveillance CC Olsen, K Kalyanam, WP Baker, DL Kunz Unmanned Systems 7 (04), 215-232, 2019 | 9 | 2019 |
