| Preliminary sizing method for hybrid-electric distributed-propulsion aircraft R De Vries, M Brown, R Vos Journal of Aircraft 56 (6), 2172-2188, 2019 | 167 | 2019 |
| Mechanism for warp-controlled twist of a morphing wing R Vos, Z Gürdal, M Abdalla Journal of Aircraft 47 (2), 450-457, 2010 | 143 | 2010 |
| Post-buckled precompressed elements: a new class of control actuators for morphing wing UAVs R Vos, R Barrett, R de Breuker, P Tiso Smart materials and structures 16 (3), 919, 2007 | 114 | 2007 |
| Introduction to transonic aerodynamics R Vos, S Farokhi Springer, 2015 | 110 | 2015 |
| Morphing wing flight control via postbuckled precompressed piezoelectric actuators R Vos, R De Breuker, R Barrett, P Tiso Journal of Aircraft 44 (4), 1060-1068, 2007 | 105 | 2007 |
| Aerodynamic interaction between propellers of a distributed-propulsion system in forward flight R de Vries, N van Arnhem, T Sinnige, R Vos, LLM Veldhuis Aerospace Science and Technology 118, 107009, 2021 | 100 | 2021 |
| A preliminary sizing method for hybrid-electric aircraft including aero-propulsive interaction effects R de Vries, MT Brown, R Vos 2018 aviation technology, integration, and operations conference, 4228, 2018 | 92 | 2018 |
| Mechanics of pressure-adaptive honeycomb and its application to wing morphing R Vos, R Barrett Smart Materials and Structures 20 (9), 094010, 2011 | 83 | 2011 |
| A method for the conceptual design of hybrid electric aircraft J Zamboni, R Vos, M Emeneth, A Schneegans AIAA scitech 2019 forum, 1587, 2019 | 73 | 2019 |
| Conceptual assessment of hybrid electric aircraft with distributed propulsion and boosted turbofans M Hoogreef, R Vos, R de Vries, LL Veldhuis AIAA Scitech 2019 Forum, 1807, 2019 | 64 | 2019 |
| Method and apparatus for pressure adaptive morphing structure R Vos, RM Barrett US Patent 8,366,057, 2013 | 64 | 2013 |
| Conceptual design and evaluation of blended-wing body aircraft M Brown, R Vos 2018 AIAA Aerospace Sciences Meeting, 0522, 2018 | 59 | 2018 |
| Range equation for hybrid-electric aircraft with constant power split R De Vries, MFM Hoogreef, R Vos Journal of Aircraft 57 (3), 552-557, 2020 | 58 | 2020 |
| A comparison of hybrid-electric aircraft sizing methods DF Finger, R de Vries, R Vos, C Braun, C Bil AIAA scitech 2020 forum, 1006, 2020 | 57 | 2020 |
| Post-buckled precompressed (PBP) actuators: enhancing VTOL autonomous high speed MAVs R Barrett, R Vos, P Tiso, R De Breuker 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials …, 2005 | 54 | 2005 |
| Preliminary sizing of a hybrid-electric passenger aircraft featuring over-the-wing distributed-propulsion R de Vries, M Hoogreef, R Vos AIAA Scitech 2019 Forum, 1811, 2019 | 53 | 2019 |
| A conceptual design and analysis method for conventional and unconventional airplanes R Elmendorp, R Vos, G La Rocca 29th Congress of the International Council of the Aeronautical Sciences 1, 2014 | 53 | 2014 |
| Post-buckled precompressed piezoelectric flight control actuator design, development and demonstration R Barrett, R McMurtry, R Vos, P Tiso, R De Breuker Smart materials and structures 15 (5), 1323, 2006 | 48 | 2006 |
| Airplane design optimization for minimal global warming impact PJ Proesmans, R Vos Journal of Aircraft 59 (5), 1363-1381, 2022 | 41 | 2022 |
| Aerodynamic design of a flying V aircraft F Faggiano, R Vos, M Baan, R Van Dijk 17th AIAA Aviation Technology, Integration, and Operations Conference, 3589, 2017 | 41 | 2017 |
Ronald M. Barrett (Gonzalez)Professor of Aerospace Engineering, The University of KansasVerified email at ku.edu
