Determining Wheel Forces and Moments on Aircraft Landing Gear with a Dynamometer Sensor †

This paper describes airfield measurement of forces and moments that act on a landing gear wheel. For the measurement, a wheel force sensor was used. The sensor was designed and built based on strain gage technology and was embedded in the left landing gear wheel of a test aircraft. The sensor is ca...

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Detalles Bibliográficos
Autores principales: Pytka, Jaroslaw, Budzyński, Piotr, Łyszczyk, Tomasz, Józwik, Jerzy, Michałowska, Joanna, Tofil, Arkadiusz, Błażejczak, Dariusz, Laskowski, Jan
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2019
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6983224/
https://www.ncbi.nlm.nih.gov/pubmed/31906132
http://dx.doi.org/10.3390/s20010227

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6983224/
https://www.ncbi.nlm.nih.gov/pubmed/31906132
http://dx.doi.org/10.3390/s20010227

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