关注
Jeffrey Taylor
Jeffrey Taylor
PhD Candidate and NASA ARMD Research Fellow, Utah State University
在 aggiemail.usu.edu 的电子邮件经过验证
标题
引用次数
引用次数
年份
Minimising induced drag with weight distribution, lift distribution, wingspan, and wing-structure weight
WF Phillips, DF Hunsaker, JD Taylor
The Aeronautical Journal 124 (1278), 1208-1235, 2020
232020
Minimum induced drag for tapered wings including structural constraints
JD Taylor, DF Hunsaker
Journal of Aircraft 57 (4), 782-786, 2020
152020
Low-fidelity method for rapid aerostructural optimisation and design-space exploration of planar wings
JD Taylor, DF Hunsaker
The Aeronautical Journal 125 (1289), 1209-1230, 2021
122021
Characterization of the Common Research Model Wing for Low-Fidelity Aerostructural Analysis
JD Taylor, DF Hunsaker
AIAA Scitech 2021 Forum, 1591, 2021
92021
Comparison of induced and parasitic drag on wings with minimum induced drag
SA Abdel-Motaleb, JD Taylor, DF Hunsaker, C Coopmans
AIAA Scitech 2019 Forum, 2120, 2019
82019
Deterring Russian Nuclear Threats with Low-Yield Nukes May Encourage Limited Nuclear War
J Taylor
Journal of Advanced Military Studies 13 (1), 207-229, 2022
42022
Numerical Algorithm for Wing-Structure Design
JD Taylor, DF Hunsaker, JJ Joo
2018 AIAA Aerospace Sciences Meeting, 1050, 2018
42018
Numerical method for rapid aerostructural design and optimization
JD Taylor, DF Hunsaker
AIAA Aviation 2020 Forum, 3175, 2020
32020
Comparison of theoretical and multifidelity optimum aerostructural solutions for wing design
JD Taylor, DF Hunsaker
Journal of Aircraft 59 (1), 103-116, 2022
22022
Methods for the Aerostructural Design and Optimization of Wings with Arbitrary Planform and Payload Distribution
JD Taylor
Utah State University, 2017
12017
Effects of Active Wing-Morphing on Aircraft Fuel Burn along Fuel-Optimal Trajectories
JD Taylor, DF Hunsaker
AIAA SCITECH 2023 Forum, 0038, 2023
2023
Multi-Fidelity Predictions for Control Allocation on the NASA Ikhana Research Aircraft to Minimize Drag
J Schoenfeld, JD Taylor, DF Hunsaker
AIAA SCITECH 2023 Forum, 0622, 2023
2023
Multidisciplinary Reference Solutions for Performance-Optimized Aircraft Wings with Tailored Aerodynamic Load Distributions
JD Taylor
Utah State University, 2022
2022
Comparison of Theoretical and High-Fidelity Aerostructural Solutions
JD Taylor, DF Hunsaker
AIAA Scitech 2021 Forum, 0067, 2021
2021
Transonic Small-Disturbance Theory/Integral Boundary Layer Airfoil Data for the Low-Fidelity Common Research Model
JD Taylor, D Hunsaker
Utah State University, 2020
2020
Minimizing Induced Drag for Tapered Wings Including Structural Constraints
JD Taylor
2020
Aerodynamic Centers of Arbitrary Airfoils Below Stall
DF Hunsaker, OD Pope, JD Taylor, J Hodson
Journal of Aircraft 56 (6), 2158-2171, 2019
2019
Minimizing Induced Drag with Weight Distribution, Wingspan, Lift Distribution, and Wing-Structure Weight
JD Taylor
2019
Optimization of Lift Distribution for Minimum Induced and Parasitic Drag Component
SA Abdel-Motaleb, JD Taylor, DF Hunsaker
2019
A Method for Evaluating the Optimum Lift Distribution and Wing Structural Requirements for a Given Payload
JD Taylor
2017
系统目前无法执行此操作,请稍后再试。
文章 1–20