[{"data":1,"prerenderedAt":139},["ShallowReactive",2],{"/resources/papers/propeller-icing":3},{"id":4,"title":5,"authors":6,"badge":47,"body":49,"cta":128,"date":129,"description":130,"extension":131,"image":132,"links":128,"meta":133,"navigation":134,"path":135,"seo":136,"stem":137,"__hash__":138},"resources/resources/papers/propeller-icing.md","Propeller Icing Test",[7,12,17,22,27,32,37,42],{"name":8,"to":9,"avatar":10},"Guillaume Catry","https://www.linkedin.com/in/guillaume-catry",{"src":11},"/img/people/guillaume-catry.webp",{"name":13,"to":14,"avatar":15},"Nicolas Bosson","https://www.linkedin.com/in/nicolas-bosson-52401b12b",{"src":16},"/img/people/nicolas-bosson.webp",{"name":18,"to":19,"avatar":20},"Sergio Marquez","https://www.linkedin.com/in/sergio-marquez1",{"src":21},"/img/people/sergio-marquez.webp",{"name":23,"to":24,"avatar":25},"Flavio Noca (PhD)","https://www.linkedin.com/in/flavio-noca",{"src":26},"/img/people/flavio-noca.webp",{"name":28,"to":29,"avatar":30},"Luca J. Bardazzi","https://www.linkedin.com/in/lucabardazzi",{"src":31},"/img/people/luca-j-bardazzi.webp",{"name":33,"to":34,"avatar":35},"Ozlem Ceyhan","https://www.linkedin.com/in/ozlemceyhan",{"src":36},"/img/people/ozlem-ceyhan.webp",{"name":38,"to":39,"avatar":40},"Pieter Jan Jordaens","https://www.linkedin.com/in/pieterjanjordaens",{"src":41},"/img/people/pieter-jan-jordaens.webp",{"name":43,"to":44,"avatar":45},"Daniele Brandolisio","https://www.linkedin.com/in/danielebrandolisio",{"src":46},"/img/people/daniele-brandolisio.webp",{"label":48},"Research Paper",{"type":50,"value":51,"toc":124},"minimark",[52,64,69,72,75,79,87,90,112,115],[53,54,55],"p",{},[56,57],"img",{"alt":58,"className":59,"src":61,"width":62,"height":63},"computer",[60],"rounded-lg","/img/propeller-icing.png",1000,350,[65,66,68],"h1",{"id":67},"abstract","Abstract",[53,70,71],{},"Among the list of harsh conditions, icing is certainly the most critical. The authors present an exploratory work to\ndevelop a method for characterizing the performances of propeller in laboratory icing conditions. This research was\nenabled by the use of a climatic chamber featuring an array of water nozzles that makes it possible to generate icing\ncondition, in combination with a windshaper – a new family of wind-generating facilities, which consists of an array of\na large number of fans (wind-pixels) that can be activated on demand to generate arbitrary winds of variable intensity\nand directions, such as uniform flows, gusts, or shear flows. Propellers were characterized with a test bench capable of\nmeasuring the thrust, motor torque, motor speed, electrical power and the weight of accreted ice.",[53,73,74],{},"Additionally, the room temperature, humidity and wind speed were also monitored separately. A visual analysis of the\naccretion of ice on the propeller that was made using short-duration flash lamps and a camera, allowed to correlate the\nperformance drop with proportion and morphology of the accreted ice on the propeller. The authors finally provide their\nobservations for a selection of test results.",[65,76,78],{"id":77},"presentation-of-the-test-setup","Presentation of the test setup",[53,80,81],{},[56,82],{"alt":83,"className":84,"src":85,"width":86},"propeller icing test setup",[60],"/img/icing_setup.jpg",400,[53,88,89],{},"The test setup includes :",[91,92,93,97,100,103,106,109],"ol",{},[94,95,96],"li",{},"Propeller, 3 blades, 9 inch in diameter, 5-inch pitch (HQProp MacroQuad 9x5x3)",[94,98,99],{},"Test stand for propulsion units – RCbenchmark 1585 by Tyto Robotics",[94,101,102],{},"1.5m x 0.75m windshaper that comprises 162 wind pixels arranged in an array of 6×3 modules",[94,104,105],{},"Water spray device – custom build by Sirris",[94,107,108],{},"Canon 5D Mk2, a full frame digital SLR camera, set at 6400 ISO, mounted with a 80mm f/1.8 lens set at maximum aperture",[94,110,111],{},"Short duration scientific strobe light (Visinst VIC 4×6 LED Array)",[53,113,114],{},"This is a joint research project between WindShape, Sirris, and HES-SO which was also supported by Tyto Robotics.",[53,116,117,118],{},"Link to the journal (AIAA Aviation Forum 2021)\n",[119,120,121],"a",{"href":121,"rel":122},"https://arc.aiaa.org/doi/abs/10.2514/6.2021-2677",[123],"nofollow",{"title":125,"searchDepth":126,"depth":126,"links":127},"",2,[],null,"2024-02-01","Performance Analysis of Rotorcraft Propulsion Units in a Combination of Wind and Icing Conditions","md",{"src":61},{},true,"/resources/papers/propeller-icing",{"title":5,"description":130},"resources/papers/propeller-icing","F2utMW0IBS_JCH_ki4cXOWeHSptDYlLltT9eYJRVs8s",1774344909558]