| Optimization of variable-camber continuous trailing-edge flap configuration for drag reduction E Ting, D Chaparro, N Nguyen, GEC Fujiwara Journal of Aircraft 55 (6), 2217-2239, 2018 | 55 | 2018 |
| A Hybrid Airfoil Design Method for Icing Wind Tunnel Tests GEC Fujiwara, BS Woodard, BD Wiberg, AJ Mortonson, MB Bragg AIAA 5th Atmospheric and Space Environments Conference, San Diego, CA, 2013 | 31 | 2013 |
| Computational and experimental ice accretions of large swept wings in the icing research tunnel GE Fujiwara, MB Bragg, S Camello, C Lum 8th AIAA Atmospheric and Space Environments Conference, 3734, 2016 | 30 | 2016 |
| 3D Swept Hybrid Wing Design Method for Icing Wind Tunnel Tests GEC Fujiwara, BD Wiberg, B Woodard, MB Bragg AIAA Atmospheric and Space Environments Conference: Aircraft Icing, 2014 | 25 | 2014 |
| Large-Scale Swept-Wing Icing Simulations in the NASA Glenn Icing Research Tunnel Using LEWICE3D B Wiberg, GEC Fujiwara, B Woodard, M Bragg AIAA AVIATION, Atlanta, GA, 2014 | 21 | 2014 |
| Comparison of computational and experimental ice accretions of large swept wings GEC Fujiwara, MB Bragg, AP Broeren Journal of Aircraft 57 (2), 342-359, 2020 | 20 | 2020 |
| Method for designing hybrid airfoils for icing wind-tunnel tests GEC Fujiwara, MB Bragg Journal of Aircraft 56 (1), 137-149, 2019 | 18 | 2019 |
| An Integral Boundary Layer Direct Method Applied to 2D Transonic Small-Disturbance Equations GE Fujiwara, D Chaparro, NT Nguyen 34th AIAA Applied Aerodynamics Conference, 3568, 2016 | 17 | 2016 |
| Development of Experimental Icing Simulation Capability for Full-Scale Swept Wings: Hybrid Design Process, Years 1 and 2 G Fujiwara, M Bragg, C Triphahn, B Wiberg, B Woodard, E Loth, A Malone, ... | 16 | 2017 |
| Aerodynamic modeling of transonic aircraft using vortex lattice coupled with transonic small disturbance for conceptual design D Chaparro, GE Fujiwara, E Ting, NT Nguyen 34th AIAA Applied Aerodynamics Conference, 3418, 2016 | 16 | 2016 |
| Transonic and Viscous Potential Flow Method Applied to Flexible Wing Transport Aircraft D Chaparro, GE Fujiwara, E Ting, NT Nguyen 35th AIAA Applied Aerodynamics Conference, 4221, 2017 | 14 | 2017 |
| A Damage Assessment for Wind Turbine Blades from Heavy Atmospheric Particles G Fiore, GEC Fujiwara, MS Selig | 14 | 2015 |
| Aeroestructural design optimization of a subsonic wing with continuous morphing trailing edge GE Fujiwara, NT Nguyen 35th AIAA Applied Aerodynamics Conference, 4218, 2017 | 13 | 2017 |
| Design of 3D swept wing hybrid models for icing wind tunnel tests GC Fujiwara University of Illinois at Urbana-Champaign, 2014 | 13 | 2014 |
| Adaptive Aeroelastic Wing Shape Optimization for High-Lift Configurations GEC Fujiwara, N Nguyen 33rd AIAA Applied Aerodynamics Conference, 2015 | 12 | 2015 |
| Method for designing three-dimensional swept hybrid wings for icing wind-tunnel tests GEC Fujiwara, MB Bragg Journal of Aircraft 56 (2), 730-746, 2019 | 11 | 2019 |
| Aerostructural design optimization of a flexible wing aircraft with continuous morphing trailing edge GE Fujiwara, NT Nguyen, E Livne, MB Bragg 2018 Multidisciplinary Analysis and Optimization Conference, 3571, 2018 | 10 | 2018 |
| 3D computational icing method for aircraft conceptual design GE Fujiwara, MB Bragg 9th AIAA Atmospheric and Space Environments Conference, 4375, 2017 | 9 | 2017 |
| Design of 3D swept wing hybrid models for icing wind tunnel tests G Camarinha Fujiwara Master's Thesis, University of Illinois at Urbana-Champaign, 2014 | 4 | 2014 |
| Design of a Human-Powered Aircraft Applying Multidisciplinary Optimization Method G Fujiwara, LM Stefanini, O Silvares SAE Technical Paper, 2013 | 2 | 2013 |
Michael B. Braggemeritus professor of Aerospace Engineering, University of Illinois, UNiversity of Washington, ohioCorreu electrònic verificat a illinois.edu
