Minimum‐series twist distributions for yawing‐moment control during pure roll*

Author:

Hunsaker Douglas F.1,Moorthamers Bruno2,Joo James J.3

Affiliation:

1. Assistant Professor, Utah State University, Logan, Utah 84322‐4130, Mechanical and Aerospace Engineering, 4130 Old Main Hill

2. PhD Candidate, Utah State University, Logan, Utah 84322‐4130, Mechanical and Aerospace Engineering, 4130 Old Main Hill

3. Senior Research Mechanical Engineer U.S. Air Force Research Laboratory Wright‐Patterson Air Force Base Ohio 45433‐7402, AFRL/RQVS, 2790 D St USA

Publisher

Wiley

Subject

Applied Mathematics,Computational Mechanics

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5. Fluid-Structure Interaction of a Variable Camber Compliant Wing

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1. Controlling roll-yaw coupling with aileron and twist design;The Aeronautical Journal;2024-03-27

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