| Nonlinear lifting-line algorithm for unsteady and post-stall conditions JN Dias 34th AIAA Applied Aerodynamics Conference, 4164, 2016 | 9 | 2016 |
| High Angle of Attack Model Identification with Compressibility Effects JN Dias AIAA Atmospheric Flight Mechanics Conference, 1477, 2015 | 9 | 2015 |
| Unsteady and Post-Stall Model Identification Using Dynamic Stall Maneuvers JN Dias AIAA Atmospheric Flight Mechanics Conference, 2705, 2015 | 8 | 2015 |
| Dynamic model of a two-stroke glow engine from experimental data JN Dias, GO Violato, CA Martins Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2012 | 7 | 2012 |
| Identification of high angle of attack aerodynamic model using flight data from spin tests JN Dias 2013 SFTE 44th Annual International Symposium, 1-26, 2013 | 5 | 2013 |
| Modal Identification of Aerodynamic Models for Spanwise Lift Distribution Control JN Dias, JE Hubbard Jr Journal of Aircraft 57 (4), 664-677, 2020 | 3 | 2020 |
| Spatial Control of Spanwise Lift Distribution for Gust Alleviation JN Dias, JE Hubbard AIAA Scitech 2019 Forum, 0108, 2019 | 3 | 2019 |
| Flight Path Reconstruction Techniques Applied to Spin Tests JN Dias AIAA Atmospheric Flight Mechanics Conference, 2559, 2014 | 3 | 2014 |
| High Angle of Attack Model Identification Without Air Flow Angle Measurements JN Dias, F Almeida AIAA Atmospheric Flight Mechanics (AFM) Conference, 4980, 2013 | 3 | 2013 |
| Recent Applications of System Identification Techniques at IPEV JN Dias, BGO Silva Journal of Aircraft 60 (5), 1398-1418, 2023 | 1 | 2023 |
| Flight-Test Determination of Longitudinal Stability Using System Identification JN Dias Journal of Aircraft 60 (5), 1659-1674, 2023 | 1 | 2023 |
| Pitot-statics Calibration using Dynamic Maneuvers and Flight-Path Reconstruction Techniques JN Dias AIAA SCITECH 2023 Forum, 0982, 2023 | 1 | 2023 |
| Flight Test Determination of Power Effects on Longitudinal Stability using System Identification JN Dias AIAA AVIATION 2022 Forum, 3637, 2022 | 1 | 2022 |
| Active Spanwise Lift Control: A Distributed Parameter Approach JN Dias, JE Hubbard Jr American Institute of Aeronautics and Astronautics, Inc., 2020 | 1 | 2020 |
| Two-point Aerodynamic Model Identification from Dynamic Wind Tunnel Tests JN Dias, RD Girardi AIAA Atmospheric Flight Mechanics Conference, 2012, 2016 | 1 | 2016 |
| Overcoming Instrumentation Limitations in Spin Tests Using Flight Path Reconstruction Techniques JN Dias 34th European Telemetry and Test Conference, 106-111, 2014 | 1 | 2014 |
| Stall Model Identification Using Flight Path Reconstruction of Multiple Maneuvers JN Dias AIAA AVIATION 2023 Forum, 3781, 2023 | | 2023 |
| Real-Time Aerodynamic Modeling of a Folding Wing Vehicle using Automatic Data Partitioning JN Dias AIAA SCITECH 2022 Forum, 1309, 2022 | | 2022 |
| Estimação de derivadas de estabilidade de uma aeronave não-tripulada através do método de mínimos quadrados ortogonais JN Dias | | 2012 |
| Equipe HoverGama ASM Fernandes, FC Martins, GO Violato, JN Dias, RB Piccinini, VG Kleine, ... | | |
James E. Hubbard Jr, NAE; FNAIOscar S. Wyatt, Jr. '45 Chair I; Hagler FellowVerified email at tamu.edu
