TY - GEN
T1 - Design of Propellers with Passive Mitigation of Coherent Tip Vortex Roll-up
AU - Kopperstad, Tove Elisabeth
AU - Borra, Akhileshwar
AU - Beusse, Andrew
AU - Kim, Cecilia
AU - Torres De Jesus, Elizabeth
AU - Saxton-Fox, Theresa
AU - Ansell, Phillip J.
N1 - Publisher Copyright:
© 2023, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2023
Y1 - 2023
N2 - A propeller design method has been developed that passively mitigates the formation of coherent tip vortex structures in the near-field of the rotor wake. Using the blade root bending moment coefficient as a surrogate variable, gradients in circulation in the radial direction are avoided in a constrained optimization problem. An additional propeller was created with an alternative optimization scheme to directly penalize gradients in shed circulation radially using a logarithmic function as a comparison. A series of wind tunnel experiments are utilized to verify design predictions and diagnose topological characteristics of the propeller vortex wakes for a conventional power-optimized design and a vortex-attenuated design. Each set of blades designs were optimized for the same specified thrust coefficient, freestream velocity, and design RPM. Thrust and torque data were taken using a test stand to verify that the design performance characteristics were achieved. Phase-locked stereoscopic particle image velocimetry data were acquired across a range of wake phase angles for the power optimized and vortex-attenuated propellers, with a single phase taken for the alternative wake optimized design. The power optimized wake showed typical coherent tip vortex rollup behavior resulting in a strong double helix wake, this is in direct contrast to the vortex-attenuated propeller which featured a distributed sheet of wake vorticity arranged in a conical spiral pattern. Additionally, the wake optimized propeller wake was shown to dissipate faster than the power optimized case. The baseline power optimized design behaved as expected with a uniform axial flow distribution, whereas the wake optimized designs both had significantly increased axial velocities near the center of rotation. This observation is due to the increased inboard induced axial and tangential velocities, promoting an accelerated swirl around the center of rotation. The interaction of the power optimized and vortex-attenuated wakes with a downstream body was also analyzed with stereo particle image velocimetry. Significant differences were observed, with large reductions in flow variability with the vortex-attenuated wake at the measurement plane analyzed.
AB - A propeller design method has been developed that passively mitigates the formation of coherent tip vortex structures in the near-field of the rotor wake. Using the blade root bending moment coefficient as a surrogate variable, gradients in circulation in the radial direction are avoided in a constrained optimization problem. An additional propeller was created with an alternative optimization scheme to directly penalize gradients in shed circulation radially using a logarithmic function as a comparison. A series of wind tunnel experiments are utilized to verify design predictions and diagnose topological characteristics of the propeller vortex wakes for a conventional power-optimized design and a vortex-attenuated design. Each set of blades designs were optimized for the same specified thrust coefficient, freestream velocity, and design RPM. Thrust and torque data were taken using a test stand to verify that the design performance characteristics were achieved. Phase-locked stereoscopic particle image velocimetry data were acquired across a range of wake phase angles for the power optimized and vortex-attenuated propellers, with a single phase taken for the alternative wake optimized design. The power optimized wake showed typical coherent tip vortex rollup behavior resulting in a strong double helix wake, this is in direct contrast to the vortex-attenuated propeller which featured a distributed sheet of wake vorticity arranged in a conical spiral pattern. Additionally, the wake optimized propeller wake was shown to dissipate faster than the power optimized case. The baseline power optimized design behaved as expected with a uniform axial flow distribution, whereas the wake optimized designs both had significantly increased axial velocities near the center of rotation. This observation is due to the increased inboard induced axial and tangential velocities, promoting an accelerated swirl around the center of rotation. The interaction of the power optimized and vortex-attenuated wakes with a downstream body was also analyzed with stereo particle image velocimetry. Significant differences were observed, with large reductions in flow variability with the vortex-attenuated wake at the measurement plane analyzed.
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U2 - 10.2514/6.2023-2614
DO - 10.2514/6.2023-2614
M3 - Conference contribution
AN - SCOPUS:85196775689
SN - 9781624106996
T3 - AIAA SciTech Forum and Exposition, 2023
BT - AIAA SciTech Forum and Exposition, 2023
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA SciTech Forum and Exposition, 2023
Y2 - 23 January 2023 through 27 January 2023
ER -