| Subsonic single aft engine (SUSAN) transport aircraft concept and trade space exploration R Jansen, CC Kiris, T Chau, LM Machado, JC Duensing, A Mirhashemi, ... AIAA SciTech 2022 Forum, 2179, 2022 | 59 | 2022 |
| A Design Exploration of Natural Laminar Flow Applications for the SUSAN Electrofan Concept MN Lynde, RL Campbell, BR Hiller AIAA Scitech 2022 Forum, 2303, 2022 | 19 | 2022 |
| Summary of the First AIAA Stability and Control Prediction Workshop TS Chyczewski, AJ Lofthouse, LM Gea, A Cartieri, BR Hiller AIAA SciTech 2022 Forum, 1680, 2022 | 17 | 2022 |
| Generation of a reduced-order model of an unmanned combat air vehicle using indicial response functions MPC van Rooij, NT Frink, BR Hiller, M Ghoreyshi, M Voskuijl Aerospace Science and Technology 95, 105510, 2019 | 14 | 2019 |
| Aeroelastic indicial response reduced-order modeling for flexible flight vehicles BR Hiller, NT Frink, WA Silva, DN Mavris Journal of Aircraft 57 (3), 469-490, 2020 | 12 | 2020 |
| Design of a Crossflow Attenuated Natural Laminar Flow Flight Test Article MN Lynde, RL Campbell, BR Hiller, LR Owens AIAA Scitech 2021 Forum, 0173, 2021 | 10 | 2021 |
| Investigation of Reduced-Order Modeling for Aircraft Stability and Control Prediction NT Frink, BR Hiller, PC Murphy, K Cunningham, GH Shah AIAA Scitech 2019 Forum, 0980, 2019 | 8 | 2019 |
| Design Exploration of a Transonic Cruise Slotted Airfoil BR Hiller, R Campbell, MN Lynde, TK Boyett AIAA AVIATION 2021 FORUM, 2525, 2021 | 6 | 2021 |
| An unsteady aerodynamics reduced-order modeling method for maneuvering, flexible flight vehicles BR Hiller Georgia Institute of Technology, 2019 | 6 | 2019 |
| Coupling Computational Fluid Dynamics with 6DOF Rigid Body Dynamics for Unsteady, Accelerated Flow Simulations ZJ Ernst, BR Hiller, CL Johnson, BE Robertson, DN Mavris 2018 AIAA Atmospheric Flight Mechanics Conference, 0291, 2018 | 6 | 2018 |
| Generation of a reduced order model of an unmanned combat air vehicle using indicial response functions M van Rooij, NT Frink, BR Hiller, M Ghoreyshi, M Voskuijl 2018 Applied Aerodynamics Conference, 2998, 2018 | 5 | 2018 |
| History and Status of the CDISC Aerodynamic Design Method RL Campbell, MN Banchy, BR Hiller AIAA SCITECH 2024 Forum, 0674, 2024 | 4 | 2024 |
| Comparison of Three Aerodynamic Analysis Software Packages Against the Army Navy Finner Projectile to Determine Fidelity Level HD Schwartz, BR Hiller, BE Robertson, DN Mavris 2018 AIAA Atmospheric Flight Mechanics Conference, 0292, 2018 | 4 | 2018 |
| Steady-state RANS Pretest CFD Comparisons for the SWiFT NTF Test B Hiller, J Luckring, D Chan AIAA SciTech Forum, 2025 | 3 | 2025 |
| Application of the CATNLF Design Method to a Transonic Transport Empennage Using CDISC BW Pomeroy, MN Banchy, RL Campbell, BR Hiller AIAA SCITECH 2024 Forum, 0676, 2024 | 3 | 2024 |
| Transonic Cruise Slotted Wing Design for Commercial Transport Aircraft using CDISC BR Hiller, RL Campbell, MN Banchy AIAA SCITECH 2024 Forum, 0677, 2024 | 2 | 2024 |
| NASA Langley FUN3D analyses in support of the 1st AIAA stability and control prediction workshop BR Hiller, MD Bozeman AIAA SCITECH 2022 Forum, 1681, 2022 | 2 | 2022 |
| Framework for Assessing Impact of Active Flow Control Technologies for Commercial Aircraft B Hiller, Y Cai, E Karagoz, C Wilhelms, I Chakraborty, SI Briceno, ... 16th AIAA Aviation Technology, Integration, and Operations Conference, 3283, 2016 | 2 | 2016 |
| An Application of CFD to Guide Forced Boundary-Layer Transition at Subsonic and Transonic Speeds for a Lambda-Wing Configuration JM Luckring, BR Hiller AIAA SCITECH 2025 Forum, 2018, 2025 | 1 | 2025 |
| CDISC Remote Design Method to Simulate Aircraft Interference Effects for the CATNLF Flight Test MN Banchy, RL Campbell, BR Hiller, MD Bozeman AIAA SCITECH 2024 Forum, 0678, 2024 | 1 | 2024 |
Neal FrinkNASAEmail verificata su nasa.gov