2020
DOI: 10.4050/jahs.65.042004
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Acoustic Characterization of Glaze and Rime Ice Structures on an Oscillating Airfoil via Fully Unsteady Simulations

Abstract: The development of low-cost and simple technologies to improve pilot awareness of icing environments is crucial to improve the safety of rotorcraft, and especially those with limited icing clearance which are admittedly operating within icing environments without full icing clearance. An acoustic characterization of glaze and rime ice structures is hereby introduced to begin to quantify different ice shape noise signatures which directly transcend from the iced performance characteristics to develop acoustic i… Show more

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Cited by 10 publications
(4 citation statements)
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“…2. PoliMIce has been developed with highly three-dimensional and unsteady problems in mind such as rotorcraft [28][29][30], making it suitable for the analysis of wavy leading edge icing. The individual solvers which are utilized for the multi-step icing simulation are hereinafter briefly outlined.…”
Section: Polimice Frameworkmentioning
confidence: 99%
“…2. PoliMIce has been developed with highly three-dimensional and unsteady problems in mind such as rotorcraft [28][29][30], making it suitable for the analysis of wavy leading edge icing. The individual solvers which are utilized for the multi-step icing simulation are hereinafter briefly outlined.…”
Section: Polimice Frameworkmentioning
confidence: 99%
“…The efficacy of the approach for predicting ice shapes on two-dimensional oscillating airfoils is highlighted in Ref. [42].…”
Section: Ice Accretionmentioning
confidence: 99%
“…PoliMIce has uniquely been developed for predicting rotorcraft ice accretion and shedding [8,9]. It has also been utilized for the innovative design of rotorcraft acoustic ice detection technologies [10,11]. PoliMIce has also been extensively developed for the simulation and robust design optimization of thermal ice protection systems (IPS) [12,13].…”
Section: Introductionmentioning
confidence: 99%