| A 2-d dynamic stall model based on a hopf bifurcation VK Truong | 48 | 1993 |
| Rotor Loads Prediction on the ONERA 7A Rotor using Loose Fluid/Structure Coupling B Ortun, M Potsdam, H Yeo, VK Truong AHS 72nd Annual Forum, West Palm Beach, Florida, USA, May 17-19, 2016, 2016 | 28 | 2016 |
| Prediction of helicopter rotor airloads based on physical modeling of 3-D unsteady aerodynamics VK Truong | 21 | 1996 |
| Modeling aerodynamics, including dynamic stall, for comprehensive analysis of helicopter rotors KV Truong Aerospace 4 (2), 21, 2017 | 20 | 2017 |
| Quantitative model for current‐voltage characteristics of metal point contacts on silicon rectifying junctions JJ Marchand, VK Truong Journal of applied physics 54 (12), 7034-7040, 1983 | 19 | 1983 |
| High-fidelity structural loads analysis of the ONERA 7A rotor H Yeo, M Potsdam, B Ortun, KV Truong Journal of Aircraft 54 (5), 1825-1839, 2017 | 18 | 2017 |
| The Free Exciton in KI. II. Coexistence with the Self Trapped Exciton T van Khiem, A Nouailhat Journal of the Physical Society of Japan 50 (1), 127-128, 1981 | 18 | 1981 |
| Structural dynamics modeling of rectangular rotor blades KV Truong, H Yeo, RA Ormiston Aerospace Science and Technology 30 (1), 293-305, 2013 | 17 | 2013 |
| Assessment of 1-D versus 3-D methods for modeling rotor blade structural dynamics H Yeo, KV Truong, R Ormiston 51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2010 | 15 | 2010 |
| Comparison of one-dimensional and three-dimensional structural dynamics modeling of advanced geometry blades H Yeo, KV Truong, RA Ormiston Journal of Aircraft 51 (1), 226-235, 2014 | 14 | 2014 |
| Indicial response approach derived from Navier-Stokes equations. Part 1: Time-invariant equilibrium state KV Truong, M Tobak | 11 | 1990 |
| An analytical model for airfoil aerodynamic characteristics over the entire 360 angle of attack range VK Truong Journal of Renewable and Sustainable Energy 12 (3), 2020 | 10 | 2020 |
| Dynamics studies of the ERATO blade, based on finite element analysis VK Truong Proceedings of the 31st European Rotorcraft Forum, 1122-1133, 2005 | 10 | 2005 |
| The Free Exciton in KI. I. Polariton Nature of the Emission T van Khiem, A Nouailhat Journal of the Physical Society of Japan 50 (1), 121-126, 1981 | 10 | 1981 |
| Towards a new generation of rotorcraft comprehensive analysis; coupling with CSM and CFD B Ortun, D Petot, KV Truong, R Ohayon | 9 | 2008 |
| Investigation of the structural blade dynamics and aeroelastic behavior of the 7A rotor S Surrey, B Ortun, VK Truong, F Wienke AHS 72 nd Annual Forum, West Palm Beach, Florida, May 17–19, 2016., 2016 | 6 | 2016 |
| Investigation of finite element approaches for rotor blade structural dynamics K Truong, H Yeo, RA Ormiston Proceedings of the 36th European Rotorcraft Forum, 2010 | 6 | 2010 |
| MODELING AERODYNAMICS FOR COMPREHENSIVE ANALYSIS OF HELICOPTER ROTORS VK Truong 42nd European Rotorcraft Forum, Lille, France, September 5-9, 2016, 2016 | 5 | 2016 |
| 2 D stall model based on Hopf bifurcation KV Truong La Recherche Aerospatiale, 55-65, 1993 | 5 | 1993 |
| The free exciton in KI and RbI: Emissions related to the triplet B exciton T van Khiem, A Nouailhat Solid State Communications 37 (7), 587-590, 1981 | 5 | 1981 |
