Holographic Airborne for Cloud Particle Imager (HACPI): Development and Applications to Icing Wind Tunnels

Instruments for icing cloud particle characterization are prerequisites for icing wind tunnels in icing physics research and aviation certification. Yet, it is challenging to measure the multiple parameters of the multiscale and multiphase icing cloud particles, especially under an extremely hostile environment. To address this issue, a holographic airborne for cloud particle imager (HACPI) has been developed for icing cloud measurement. With the merit of 3-D imaging of holography, HACPI has the capability of simultaneously measuring particle morphology, size distribution, median volume diameter (MVD), and liquid water content (LWC), with a graphical user interface (GUI) software for remote control and real-time processing through parallel reconstruction. Aerodynamic simulations indicate relatively uniform flow characteristics within a sampling depth of 46 mm. The developed HACPI is applied to three industrial icing wind tunnels with test section scales ranging from <inline-formula xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink"> <tex-math notation="LaTeX">$0.6\times 0.6$ </tex-math></inline-formula> to <inline-formula xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink"> <tex-math notation="LaTeX">$3.0\times 2.0$ </tex-math></inline-formula>m. The elaborative designs of optical-mechanical–electronic-thermal integrations evidenced HACPI’s robust performance in high-speed wind up to ~200 m/s and low static temperature down to −30 °C. Results show that HACPI can accurately measure the icing clouds in the Code of Federal Regulations Title 14 Part 25 Appendix C, the bimodal supercooled large droplet (SLD) conditions in Appendix O, and the ice crystals in the Code of Federal Regulations Title 14 Part 33 Appendix D, with accuracies verified by side-by-side comparisons to certificated commercial instruments. HACPI has been demonstrated to be a powerful instrument for icing cloud measurement in icing wind tunnels and can be extended to other ground simulation facilities as well as aviation certification.

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Publication Details

Journal
IEEE Transactions on Instrumentation and Measurement
Published
2024-11-13
DOI
https://doi.org/10.1109/tim.2024.3497171
Citations
1
Primary Topic
Spacecraft and Cryogenic Technologies
Type
article
Field-Weighted Citation Impact
1.30

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article

Holographic Airborne for Cloud Particle Imager (HACPI): Development and Applications to Icing Wind Tunnels

Yingchun Wu, Boyi Wang, Xuecheng Wu, Zixu Wang et al.
1 citations
IEEE Transactions on Instrumentation and Measurement
Spacecraft and Cryogenic Technologies
1.30
article

Holographic Airborne for Cloud Particle Imager (HACPI): Development and Applications to Icing Wind Tunnels

Yingchun Wu, Boyi Wang, Xuecheng Wu, Zixu Wang, Xinyuan Huang, Zhiqiang Zhang, Letian Zhang, Xiangdong Guo, Xiaodan Lin, Si Li
article en
1 citations

Abstract

Instruments for icing cloud particle characterization are prerequisites for icing wind tunnels in icing physics research and aviation certification. Yet, it is challenging to measure the multiple parameters of the multiscale and multiphase icing cloud particles, especially under an extremely hostile environment. To address this issue, a holographic airborne for cloud particle imager (HACPI) has been developed for icing cloud measurement. With the merit of 3-D imaging of holography, HACPI has the capability of simultaneously measuring particle morphology, size distribution, median volume diameter (MVD), and liquid water content (LWC), with a graphical user interface (GUI) software for remote control and real-time processing through parallel reconstruction. Aerodynamic simulations indicate relatively uniform flow characteristics within a sampling depth of 46 mm. The developed HACPI is applied to three industrial icing wind tunnels with test section scales ranging from <inline-formula xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink"> <tex-math notation="LaTeX">$0.6\times 0.6$ </tex-math></inline-formula> to <inline-formula xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink"> <tex-math notation="LaTeX">$3.0\times 2.0$ </tex-math></inline-formula>m. The elaborative designs of optical-mechanical–electronic-thermal integrations evidenced HACPI’s robust performance in high-speed wind up to ~200 m/s and low static temperature down to −30 °C. Results show that HACPI can accurately measure the icing clouds in the Code of Federal Regulations Title 14 Part 25 Appendix C, the bimodal supercooled large droplet (SLD) conditions in Appendix O, and the ice crystals in the Code of Federal Regulations Title 14 Part 33 Appendix D, with accuracies verified by side-by-side comparisons to certificated commercial instruments. HACPI has been demonstrated to be a powerful instrument for icing cloud measurement in icing wind tunnels and can be extended to other ground simulation facilities as well as aviation certification.

IEEE Transactions on Instrumentation and MeasurementVol. 74
Commercial Aircraft Corporation of China (China) (CN), China Aerodynamics Research and Development Center (CN), State Key Laboratory of Clean Energy Utilization, Zhejiang University (CN)
National Natural Science Foundation of China, Natural Science Foundation of Jiangsu Province for Distinguished Young Scholars
Affordable and clean energy
Openalex Percentile: Top 12%
Spacecraft and Cryogenic Technologies
1.30
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