Tesis sobre el tema "NOISE LANDING GEAR"
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Liu, Wen. "Numerical investigation of landing gear noise". Thesis, University of Southampton, 2011. https://eprints.soton.ac.uk/210942/.
Texto completoWang, Meng. "High-order numerical investigations into landing gear wheel noise". Thesis, University of Southampton, 2017. https://eprints.soton.ac.uk/416431/.
Texto completoBoorsma, Koen. "Aeroacoustic control of landing gear noise using perforated fairings". Thesis, University of Southampton, 2008. https://eprints.soton.ac.uk/66081/.
Texto completoFattah, Ryu. "The noise generation by a main landing gear door". Thesis, University of Southampton, 2016. https://eprints.soton.ac.uk/390837/.
Texto completoLopes, Leonard Vincent Brentner Kenneth S. "A new approach to complete aircraft landing gear noise prediction". [University Park, Pa.] : Pennsylvania State University, 2009. http://etda.libraries.psu.edu/theses/approved/WorldWideIndex/ETD-4401/index.html.
Texto completoRavetta, Patricio A. "LORE Approach for Phased Array Measurements and Noise Control of Landing Gears". Diss., Virginia Tech, 2005. http://hdl.handle.net/10919/29975.
Texto completoPh. D.
Remillieux, Marcel Christophe. "Aeroacoustic Study of a Model-Scale Landing Gear in a Semi-Anechoic Wind Tunnel". Thesis, Virginia Tech, 2007. http://hdl.handle.net/10919/31674.
Texto completoMaster of Science
Van, Mierlo Koen. "Computational analysis of the flow field and noise radiation of a generic main landing gear configuration". Thesis, University of Southampton, 2014. https://eprints.soton.ac.uk/388076/.
Texto completoBouchouireb, Hamza. "Identification and modelling of noise sources on a realisticnose landing gear using phased array methods applied tocomputational data". Thesis, KTH, MWL Marcus Wallenberg Laboratoriet, 2017. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-209186.
Texto completoČavojský, Tomáš. "Návrh podvozku malého dvoumístného letounu". Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2021. http://www.nusl.cz/ntk/nusl-442821.
Texto completoNguyen, Thoai D. "Finite Element Analysis of a Nose Gear During Landing". UNF Digital Commons, 2010. http://digitalcommons.unf.edu/etd/215.
Texto completoTrojánek, Tomáš. "Návrh podvozku malého dvoumístného letounu". Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2018. http://www.nusl.cz/ntk/nusl-377755.
Texto completoNovák, Josef. "Návrh podvozku VUT200 TwinCobra". Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2015. http://www.nusl.cz/ntk/nusl-232017.
Texto completoBaláš, Martin. "Pevnostní kontrola a topologická optimalizace dílu podvozku letounu". Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2020. http://www.nusl.cz/ntk/nusl-417462.
Texto completoKewley, Sarah Elizabeth. "Parametric study into the shimmy dynamics of a nose landing gear-fuselage model". Thesis, University of Bristol, 2015. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.702149.
Texto completoBednář, Peter. "Návrh příďového podvozku pro letouny řady Zlín 40". Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2021. http://www.nusl.cz/ntk/nusl-442851.
Texto completoVodička, Petr. "Návrh elektro-hydraulické soustavy pro ovládání příďového podvozku malého dopravního letounu". Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2017. http://www.nusl.cz/ntk/nusl-318402.
Texto completoPauliny, Jozef. "Návrh podvozku čtyřmístného jednomotorového letounu". Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2014. http://www.nusl.cz/ntk/nusl-231654.
Texto completoSONI, AMIT KUMAR. "FATIGUE LIFE ESTIMATION OF LANDING GEARS OF FIGHTER AIRCRAFT USING FINITE ELEMENT ANALYSIS". Thesis, 2012. http://dspace.dtu.ac.in:8080/jspui/handle/repository/13953.
Texto completoThe Total Technical Life (TTL) of fighter aircraft “Article 29L” is 1800 flying hrs. However the TTL of Main Landing Gear (MLG) and Nose Landing Gear (NLG) is only 2000 landing. Considering average sortie duration of 45 minutes, the life of LGs should have been ideally 2400 landings. So there is need to increase the life of LGs. In older days the stress analysis and life extension study was carried out considering the experimental stress analysis approach and testing, which is time consuming and require huge testing setup. In order to bridge this gap and to reduce the effort, it is proposed to estimate the life of the under carriage by Integrated Approach of Finite Element (FE) Analysis. The determination of the fatigue life of an engineering structure is based on two precepts. These are knowledge of the structure itself and knowledge of how that structure is loaded. The information required for fully understanding these two singularly complicated items is significant hence utmost care is taken to estimation of life of LGs. In this work Finite Element (FE) Analysis 3-D geometric modeling developed using CATIA software. The assembly model was imported in PATRAN software and 3-D mesh was generated using HYPERMESH. Connectivity between the components is provided using the surface to surface contact element. Contact elements are capable of transferring the displacement as per contact status and stiffness of contacting body. The FE model was solved using NASTRAN software for stress and displacement, as per fatigue test load data available. Further fatigue analysis has been carried out using MSC Fatigue software for fatigue life estimation. To validate FE stress analysis, results were compared with classical calculations and Rejuvenation zones of MLG. Thus determine cumulative fatigue damage hot spots can be rejuvenated locally and more no of landing (life of LGs) can be extended accordingly and avoid the experimental stress analysis approach and testing for life extension.
Shuo-ChenKao y 高碩辰. "On the Mechanism Design of Nose Landing Gears". Thesis, 2019. http://ndltd.ncl.edu.tw/handle/ex3cxd.
Texto completoSilva, José Miguel Casaca Faria. "Development of a nose landing gear of an unmanned aircraft (RPAS)". Master's thesis, 2017. https://hdl.handle.net/10216/103432.
Texto completoSilva, José Miguel Casaca Faria. "Development of a nose landing gear of an unmanned aircraft (RPAS)". Dissertação, 2017. https://repositorio-aberto.up.pt/handle/10216/103432.
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