Fujiwara, G. E., Bragg, M. B., and Broeren, A. P., “Comparison of Computational and Experimental Ice Accretions of Large Swept Wings,” Journal of Aircraft, Vol. 57, No. 2 (2020), pp. 342-359, doi: 10.2514/1.C035631.

Fujiwara, G. E., and Bragg, M. B., “Method for Designing Three-Dimensional Swept Hybrid Wings for Icing Wind-Tunnel Tests,” Journal of Aircraft, Vol. 56, No. 2 (2019), pp. 730-746, doi: 10.2514/1.C035136.

Ting, E., Chaparro, D., Nguyen, N. T., and Fujiwara, G. E., “Optimization of Variable Camber Continuous Trailing Edge Flap Configuration for Drag Reduction,” Journal of Aircraft, Vol. 55, No. 6 (2018), pp. 2217-2239, doi: 10.2514/1.C034810.

Fujiwara, G. E., and Bragg, M. B., “Method for Designing Hybrid Airfoils for Icing Wind-Tunnel Tests,” Journal of Aircraft, Vol. 56, No. 1 (2019), pp. 137-149, doi: 10.2514/1.C034987.

Fujiwara, G. E., Nguyen, N. T., Livne, E., and Bragg, M., “Aerostructural Design Optimization of a Flexible Wing Aircraft with Continuous Morphing Trailing Edge,” In 19th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Atlanta, GA, June 2018, AIAA 2018-3571, doi: 10.2514/6.2018-3571.

Fujiwara, G. E., and Nguyen, N. T., “Aeroestructural Design Optimization of a Subsonic Wing with Continuous Morphing Trailing Edge,” In 35th AIAA Applied Aerodynamics Conference, Denver, CO, June 2017, AIAA 2017-4218, doi: 10.2514/6.2017-4218.

Chaparro, D., Fujiwara, G. E., Ting, E., and Nguyen, N.T., “Transonic and Viscous Potential Flow Method Applied to Flexible Wing Transport Aircraft,” In 35th AIAA Applied Aerodynamics Conference, Denver, CO, June 2017, AIAA 2017-4221, doi: 10.2514/6.2017-4221.

Fujiwara, G. E., and Bragg, M. B., “3D Computational Icing Method for Aircraft Conceptual Design,” In 9th AIAA Atmospheric and Space Environments Conference, Denver, CO, June 2017, AIAA 2017-4375, doi: 10.2514/6.2017-4375.

Fujiwara, G., Bragg, M., Triphahn, C., Wiberg, B., Woodard, B., Loth, E., Malone, A., Paul, B., Pitera, D., Wilcox, P., Khodadoust, A., “Development of Experimental Icing Simulation Capability for Full-Scale Swept Wings Hybrid Design Process, Years 1 and 2,” doi: NASA/CR–2017-219573.

Fujiwara, G. E., Chaparro, D., and Nguyen, N. T., “An Integral Boundary Layer Direct Method Applied to 2D Transonic Small-Disturbance Equations,” In 34th AIAA Applied Aerodynamics Conference, Washington, DC, June 2016, AIAA 2016-3568, doi: 10.2514/6.2016-3568.

Chaparro, D., Fujiwara, G. E., Ting, E., and Nguyen, N. T., “Aerodynamic Modeling of Transonic Aircraft Using Vortex Lattice Coupled with Transonic Small Disturbance for Conceptual Design,” In 34th AIAA Applied Aerodynamics Conference, Washington, DC, June 2016, AIAA 2016-3418, doi: 10.2514/6.2016-3418.

Fujiwara, G. E., Bragg, M. B., Camello, S., and Lum, C., “Computational and Experimental Ice Accretions of Large Swept Wings in the Icing Research Tunnel,” In 8th AIAA Atmospheric and Space Environments Conference, Washington, DC, June 2016, AIAA 2016-3734, doi: 10.2514/6.2016-3734.

Fujiwara, G. E., and Nguyen, N. T., “Adaptive Aeroelastic Wing Shape Optimization for High-Lift Configurations,” In 33rd AIAA Applied Aerodynamics Conference, Dallas, TX, AIAA 2015-2420, doi: 10.2514/6.2015-2420.

Fiore, G., Camarinha Fujiwara, G. E., and Selig, M. S., “A Damage Assessment for Wind Turbine Blades from Heavy Atmospheric Particles,” In 53rd AIAA Aerospace Sciences Meeting, Kissimmee, FL, AIAA 2015-1495, doi: 10.2514/6.2015-1495.

Camarinha Fujiwara, Gustavo. "Design of 3D swept wing hybrid models for icing wind tunnel tests." M.S. Thesis, University of Illinois at Urbana-Champaign, 2015.

Fujiwara, G. E., Wiberg, B. D., Woodard, B., and Bragg, M., “3D Swept Hybrid Wing Design Method for Icing Wind Tunnel Tests,” In 6th AIAA Atmospheric and Space Environments Conference, Atlanta, GA, AIAA 2014-2616, doi: 10.2514/6.2014-2616.

Wiberg, B. D., Fujiwara, G. E., Woodard, B., and Bragg, M., “Large-Scale Swept-Wing Icing Simulations in the NASA Glenn Icing Research Tunnel Using LEWICE3D,” In 6th AIAA Atmospheric and Space Environments Conference, Atlanta, GA, AIAA 2014-2617, doi: 10.2514/6.2014-2617.

Fujiwara, G., Stefanini, L. M., and Silvares, O., “Design of a Human-Powered Aircraft Applying Multidisciplinary Optimization Method,” SAE 2013 AeroTech Congress & Exhibition Montreal, Canada, Technical Paper No. 2013-01-2318, doi: 10.4271/2013-01-2318.

Fujiwara, G. E., Woodard, B., Wiberg, B., Mortonson, A. J., and Bragg, M., “A Hybrid Airfoil Design Method for Icing Wind Tunnel Tests,” In 5th AIAA Atmospheric and Space Environments Conference, San Diego, CA, AIAA 2013-2826, doi: 10.2514/6.2013-2826.

Fujiwara, Gustavo Eidji Camarinha, "Projeto de Aeronave Movida a Propulsão Humana," Undergraduate Thesis, Polytechnic School of University of Sao Paulo, 2011.

Aerial vehicle and aerial vehicle systems
WO WO2024182492A1  Gustavo Eidji Camarinha FUJIWARA  Zipline International Inc.
Priority 2023-03-02 • Filed 2024-02-28 • Published 2024-09-06