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Tesi sul tema "Blages"

Autore: Grafiati

Pubblicato: 4 giugno 2021

Ultima modifica: 1 febbraio 2022

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1

Weldhagen, Gerhard Frederick. "Laboratory Detection and Gene Cassette Stability of the Novel Extended-Spectrum Beta-Lactamase, GES-2 from Pseudomonas aeruginosa." Thesis, University of Pretoria, 2004. http://hdl.handle.net/2263/29221.

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Extended-spectrum beta-lactamases (ESBLs) in Pseudomonas aeruginosa tend to be geographically scattered, such as GES-2, which partially compromises the efficacy of imipenem. The G170N mutation, ascribed to a CC to AA base pair substitution on positions 493-494 of the blaGES-2 coding region, distinguishes this ESBL from blaGES-1 and the blaIBC-type genes, making it an ideal target for developing a novel sequence-specific, peptide nucleic acid (PNA)-based, multiplex-PCR detection method. Utilizing two primer pairs in conjunction with a PNA probe, this novel method delivered accurate identificati

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2

Ruiz, Leonardo Guizilini Plazas [UNESP]. "Resistência aos beta-lactâmicos e detecção dos genes blashv, blatem, blactx-m e blages em Enterobacteriaceae isoladas de efluentes hospitar e comunitário em um município do noroeste paulista." Universidade Estadual Paulista (UNESP), 2010. http://hdl.handle.net/11449/94851.

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Made available in DSpace on 2014-06-11T19:27:21Z (GMT). No. of bitstreams: 0 Previous issue date: 2010-10-26Bitstream added on 2014-06-13T20:35:44Z : No. of bitstreams: 1 ruiz_lgp_me_sjrp.pdf: 1611382 bytes, checksum: e9dd037c5c8d3c485f14ae8a1628ab2e (MD5)<br>As Enterobacteriaceae constituem um importante grupo de patógenos humanos, causadores de infecções hospitalares e comunitárias. Nestas bactérias, a produção de beta-lactamases de espectro estendido (ESBL) é um dos principais mecanismos de resistência aos antibióticos, e responsável pela falha da terapia antimicrobiana. Enterobactérias r

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3

Ruiz, Leonardo Guizilini Plazas. ""Resistência aos beta-lactâmicos e detecção dos genes blashv, blatem, blactx-m e blages em Enterobacteriaceae isoladas de efluentes hospitar e comunitário em um município do noroeste paulista" /." São José do Rio Preto : [s.n.], 2010. http://hdl.handle.net/11449/94851.

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Orientador: Mara Corrêa Lelles Nogueira<br>Banca: Doroti de Oliveira Garcia<br>Banca: Fátima Pereira de Souza<br>Resumo: As Enterobacteriaceae constituem um importante grupo de patógenos humanos, causadores de infecções hospitalares e comunitárias. Nestas bactérias, a produção de beta-lactamases de espectro estendido (ESBL) é um dos principais mecanismos de resistência aos antibióticos, e responsável pela falha da terapia antimicrobiana. Enterobactérias resistentes a antibióticos são encontradas em águas superficiais e apresentam alta prevalência em águas servidas, inclusive pós-tratamento. Es

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4

Braga, Jisbaque Melo. "Prevalência e sensibilidade antimicrobiana de escherichia coli e klebsiella pneumoniae isoladas de infecções nosocomiais no hospital regional norte em sobral/ce e detecção genética de blatem, blashv blactx-m e blages em espécimes produtores de betalactamase de espectro estendido (esbl)." reponame:Repositório Institucional da UFC, 2016. http://www.repositorio.ufc.br/handle/riufc/22878.

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BRAGA, J.M. Prevalência e sensibilidade antimicrobiana de escherichia coli e klebsiella pneumoniae isoladas de infecções nosocomiais no hospital regional norte em sobral/ce e detecção genética de blatem, blashv blactx-m e blages em espécimes produtores de betalactamase de espectro estendido (esbl). 2016. 101f. Dissertação (Mestrado em Ciências da Saúde) – Campus de Sobral, Universidade Federal do Ceará, Sobral, 2016.<br>Submitted by Mestrado Ciências da Saúde (ppgcsufcsobral@gmail.com) on 2017-05-25T14:15:01Z No. of bitstreams: 1 2016_dis_jmbraga.pdf: 4368780 bytes, checksum: f1881d9ef6

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5

Blagoev, Blagoy [Verfasser]. "Arbeitszeitregime im Lock-in? : Eine pfadtheoretische Untersuchung der Persistenz überlanger Arbeitszeiten in einem Beratungsunternehmen / Blagoy Blagoev." Berlin : Freie Universität Berlin, 2016. http://d-nb.info/1099282845/34.

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6

Hettasch, Georg. "Optimization of fir-tree-type turbine blade roots using photoelasticity." Thesis, Stellenbosch : University of Stellenbosch, 1992. http://hdl.handle.net/10019.1/993.

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Thesis (MEng.)-- University of Stellenbosch, 1992. 140 leaves on single pages, preliminary pages i-xi and numbered pages 1-113. Includes bibliography. Digitized at 600 dpi grayscale to pdf format (OCR),using an Bizhub 250 Konica Minolta Scanner and at 300 dpi grayscale to pdf format (OCR), using a Hp Scanjet 8250 Scanner.<br>Thesis (MEng (Mechanical and Mechatronic Engineering))--University of Stellenbosch, 1992<br>ENGLISH ABSTRACT: The large variety of turbo-machinery blade root geometries in use in industry prompted the question if a optimum geometry could be found. An optimum blade root w

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7

Bose, Anushika. "Birds & Blades." Doctoral thesis, Humboldt-Universität zu Berlin, 2021. http://dx.doi.org/10.18452/22458.

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Kollisionen von Vögeln mit Windturbinen haben sich zu einer bedenklichen Quelle für die Gefährdung besonders von Populationen seltenerer Vogelarten entwickelt. Allerdings wird im Allgemeinen auch bestätigt, dass die Nutzung der Windenergie unverzichtbar ist. Das Hauptziel dieser Arbeit war es, die Relevanz der Wechselwirkungen zu verstehen, die zwischen technischen Infrastrukturen und den von Kollisionen betroffenen Vogelarten auf der Landschaftsebene stattfinden. Da sowohl von der Landschaft beeinflusst werden. Unter Nutzung der durch gezielte Nachsuche gefundenen Opfer der am häufigsten von

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8

Drude, Matthias, and Else Lasker-Schüler. "Mein blaues Klavier: (1986)." Matthias Drude, 2018. https://slub.qucosa.de/id/qucosa%3A17093.

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9

Birgmark, Anja. "Wear of Coater Blades." Thesis, Karlstads universitet, Fakulteten för teknik- och naturvetenskap, 2013. http://urn.kb.se/resolve?urn=urn:nbn:se:kau:diva-27183.

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10

Medd, Adam Jon. "Inverse design of turbomachinery blades." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 1998. http://www.collectionscanada.ca/obj/s4/f2/dsk2/tape17/PQDD_0010/MQ34391.pdf.

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11

Ireland, Peter. "Internal cooling of turbine blades." Thesis, University of Oxford, 1987. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.235870.

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12

Purvis, Richard. "Rotor blades and ground effect." Thesis, University College London (University of London), 2002. https://ueaeprints.uea.ac.uk/20790/.

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This thesis uses numerical, asymptotic and flow structural techniques to examine various aspects of rotor blade flows and ground effect. It explores two- and three-dimensional flows, generally concentrating upon regimes that have a degree of relevance to typical rotor blade flows. Chapter 2 considers, as a first step towards understanding a general rotor blade system in ground effect, a finite rotating disc near horizontal ground. More specifically, it concentrates on determining the layer shape beyond the disc rim that, due to the presence of the ground, cannot remain flat without violating a

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13

Bose, Anushika [Verfasser]. "Birds & Blades / Anushika Bose." Berlin : Humboldt-Universität zu Berlin, 2021. http://d-nb.info/1229435301/34.

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14

Pursell, Mark Edward. "Two Blades Come Together: Stories." Master's thesis, University of Central Florida, 2007. http://digital.library.ucf.edu/cdm/ref/collection/ETD/id/3932.

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This collection of seven short stories details the emotional triumphs and complications of characters whose lives are altered by issues of sexuality and disconnection. An adolescent girl feels her father slipping away from her and, in turn, willfully destroys the imaginary world of the boy she babysits; a speech therapist struggles to make headway with a young patient while finding himself unable to communicate with his ex-lover; a gay poet cheats on his boyfriend in a desperate attempt to fuel his failing art. The dramatis personae of Two Blades Come Together is comprised of individuals who s

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15

Dong, Yuan. "Boundary layers on compressor blades." Thesis, University of Cambridge, 1988. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.278266.

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16

Hart, M. "Boundary layers on turbine blades." Thesis, University of Cambridge, 1985. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.305764.

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17

Moore, Timothy David. "Automated inspection of turbine blades." Thesis, University of Manchester, 2003. https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.762419.

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18

Kee, Kim Chung. "Particle impacts on impeller blades." Thesis, University of Cambridge, 1999. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.624407.

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19

Zimmer, Aline Katharina. "Investigation of the impact of turbine blade geometry on near-field microwave blade tip time of arrival measurements." Thesis, Atlanta, Ga. : Georgia Institute of Technology, 2008. http://hdl.handle.net/1853/26558.

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Thesis (M. S.)--Aerospace Engineering, Georgia Institute of Technology, 2009.<br>Committee Chair: Jagoda, Jechiel; Committee Co-Chair: Jacobs, Laurence; Committee Member: Seitzman, Jerry. Part of the SMARTech Electronic Thesis and Dissertation Collection.

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20

Gase, Zachary M. "Below-Rated Control of Swept-Blade Wind Turbines." Scholarly Commons, 2016. https://scholarlycommons.pacific.edu/uop_etds/225.

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Modelling studies have shown that 1.5 and 3.0 MW wind turbines with blade sweep have an increased annual energy production (AEP) of approximately 5% when compared to straight-blade wind turbines. The objective of the research was to further increase below-rated, variable speed, power capture when using swept-blades. When operating in the variable speed region, the turbine’s torque is proportional to the square of the generator speed, and k is the proportionality constant (T = kΩ 2 ). Initial studies indicated that the value of k needed to be lowered from the original value to increase AEP. Thi

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21

Höyland, Jörg. "Challenges for large wind turbine blades." Doctoral thesis, Norges teknisk-naturvitenskapelige universitet, Institutt for produktutvikling og materialer, 2010. http://urn.kb.se/resolve?urn=urn:nbn:no:ntnu:diva-13545.

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With global climate problems receiving increasingly international political attention,most European nations are looking for sources of renewable energy. Wind turbines area promising source of renewable energy and their numbers have steadily increasedsince the introduction of the modern wind turbine in the 1970s. The largest units todayhave a rated power of 7 MW and blades ranging up to 62.5 m in length. Offshore windturbines have access to stronger winds with less turbulence, thereby increasing theenergy output of each unit. Offshore turbines will also have a lesser environmentalimpact than on

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22

Marinus, Benoît. "Multidisciplinary optimization of aircraft propeller blades." Phd thesis, Ecole Centrale de Lyon, 2011. http://tel.archives-ouvertes.fr/tel-00692363.

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Open rotors are known to have significant advantages in terms of propulsive efficiency. These advantages translate directly in reduced fuel burn so that they nowadays benefit from a surge of interest. At the same time, recent advances in numerical simulations make the application of multidisciplinary optimization for the demanding design of transonic propeller blades, an affordable option. Therefore, an optimization method in which the performance objectives of aerodynamics, aeroacoustics and aeroelasticity compete against each other, is developed and applied for the design of high-speed singl

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23

Fulton, Mark V. "Stability of elastically tailored rotor blades." Diss., Georgia Institute of Technology, 1992. http://hdl.handle.net/1853/12248.

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24

Rogalsky, Timothy P. "Aerodynamic shape optimization of fan blades." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 1999. http://www.collectionscanada.ca/obj/s4/f2/dsk2/ftp01/MQ35083.pdf.

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25

Nowak, William J. "Fatigue stress analysis of turbine blades /." Online version of thesis, 2007. http://hdl.handle.net/1850/5467.

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26

He, Li. "Unsteady flows around oscillating turbomachinery blades." Thesis, University of Cambridge, 1990. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.385407.

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27

Hamakhan, Idres Azzat. "Design of high efficiency turbomachinery blades." Thesis, Queen Mary, University of London, 2010. http://qmro.qmul.ac.uk/xmlui/handle/123456789/618.

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28

Burman, Jörgen. "Design optimisation of aeroengine compressor blades." Licentiate thesis, Luleå, 2001. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-25824.

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Optimisation of multistage axial compressors is a time-demanding challenge in large need of effective methods. Traditionally, the design has been based on "trial-and-error" procedures, which count on the skills and experience of the designer to suggest redesigns that are likely to yield improvements. While design by "trial-and-error" usually yield acceptable solutions, automatic shape optimisation will assist in finding the optimal design and shorten the design cycle. This thesis considers issues that have to be solved before automatic shape optimisation of compressor blades can be performed,

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29

Bolger, John Jude. "Three dimensional design of compressor blades." Thesis, University of Cambridge, 1999. https://www.repository.cam.ac.uk/handle/1810/251477.

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30

Pearce, Robert. "Internal cooling for HP turbine blades." Thesis, University of Oxford, 2016. https://ora.ox.ac.uk/objects/uuid:832038c9-e934-413d-bbb5-336ab4775055.

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Modern gas turbine engines run at extremely high temperatures which require the high pressure turbine blades to be extensively cooled in order to reach life requirements. This must be done using the minimum amount of coolant in order to reduce the negative impacts on the cycle efficiency. In the design process the cooling configuration and stress distribution must be carefully considered before verification of the design is conducted. Improvements to all three of these blade design areas are presented in this thesis which investigates internal cooling systems in the form of ribbed, radial pass

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31

Ricquemaque, Lore. "FEM model of impacts on blades." Thesis, KTH, Kraft- och värmeteknologi, 2016. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-185693.

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In-service support engineers often have to answer derogations requests regarding impacts on compressor blades. The stress concentration factor is a physical quantity helping them to take the decisions : it is a measure of the local increase of the stress due to the impact. Several techniques already exist to derive it like Petersons' abaci giving it regarding the geometrical parameters of the impact. They are user friendly but conservative in practice. The most accurate method is zoom-calculation : a Finite Element Model is created to precisely measure the stress concentration factor. This eff

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32

Dias, Bruno Ricardo Barros. "Adaptive gurney flap for rotor blades." Master's thesis, Universidade da Beira Interior, 2013. http://hdl.handle.net/10400.6/1976.

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Desde muito tempo vários esforços tem sido feitos de maneira a optimizar o rotor dos helicópteros com o objectivo de reduzir a emissão de poluentes. Durante vários anos foram feitas várias optimizações estrutrais na pá do rotor. Estudos recentes numéricos e experimentais mostram que para melhor a performance do rotor várias considerações aerodinâmicas têm que ser levadas em conta. O principal objectivo deste trabalho é estudar e optimizar um mecanismo preliminar constituído por um flap dinâmico que consiga controlar a camada limite na pá. O flap escolhido foi o Gurney Flap, desenvolvido nos

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33

Li, Leihong. "Structural design of composite rotor blades with consideration of manufacturability, durability, and manufacturing uncertainties." Diss., Atlanta, Ga. : Georgia Institute of Technology, 2008. http://hdl.handle.net/1853/24757.

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Thesis (Ph.D.)--Aerospace Engineering, Georgia Institute of Technology, 2009.<br>Committee Chair: Hodges, Dewey H.; Committee Member: Bauchau, Olivier A.; Committee Member: Johnson, Ellis; Committee Member: Makeev, Andrew; Committee Member: Volovoi, Vitali V.

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34

Raubenheimer, Gert. "Vibration excitation of axial compressor rotor blades." Thesis, Stellenbosch : Stellenbosch University, 2011. http://hdl.handle.net/10019.1/17987.

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Thesis (MScEng)--Stellenbosch University, 2011.<br>ENGLISH ABSTRACT: Turbomachines are exposed to several environmental factors which may cause failure of components. One of these factors, high cycle fatigue, is often caused by blade utter. This thesis forms part of a project of the European Seventh Framework Programme (FP7), called project Future. Project Future is doing theoretical and experimental investigation into the occurrence of utter in turbomachinery. The objective of this thesis was to evaluate the effectiveness of a gas injection system as a means of exciting vibrations on

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35

Turnock, Wingyan Wong. "Impact response of composite helicopter rotor blades." Thesis, Cranfield University, 2004. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.422188.

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36

Khan, Fahd. "Investigating into advanced coatings for bandsaw blades." Thesis, Northumbria University, 2011. http://nrl.northumbria.ac.uk/36301/.

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Bandsawing is an important metal cutting operation carried out in a variety of industries in order to remove raw material for secondary operations. Due to its continuous cutting action, bandsawing has over taken other cutting processes such as power hack sawing and circular sawing. Bandsawing operation offers numerous advantages such as high cutting rate, low kerf loss, longer tool life and high automation possibilities, due to its efficient and continuous cutting action. It is costly and time-consuming to test the wear of the full bandsaw products on a full-scale bandsaw machine. In order to

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37

Dow, Eric Alexander. "Robust design and tolerancing of compressor blades." Thesis, Massachusetts Institute of Technology, 2015. http://hdl.handle.net/1721.1/97351.

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Thesis: Ph. D., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2015.<br>Cataloged from PDF version of thesis.<br>Includes bibliographical references (pages 147-152).<br>Variations in the geometry of compressor blades can be introduced by variability in the manufacturing process or by in-service erosion. Recent research efforts have focused on characterizing the impacts of this geometric variability on turbomachinery performance and designing blade geometries whose performance is robust to this variability. Relatively little work has been done to specify the

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38

Gubran, Ahmed. "Vibration diagnosis of blades of rotating machines." Thesis, University of Manchester, 2015. https://www.research.manchester.ac.uk/portal/en/theses/vibration-diagnosis-of-blades-of-rotating-machines(40f1d466-b393-42f6-a65a-e16801f06920).html.

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Rotating blades are considered to be the one of the most common cause of failures in rotating machinery. Blade failure modes normally occur as a result of cracks due to unexpected operating conditions, which are normally caused by accidents of foreign objects damage, high cycle fatigue, blade rubbing, blade root looseness, and degradation from erosion and corrosion. Thus, detection of blade faults has an important role in reducing blade related failures and allowing repairs to be scheduled for the machinery. This in turn will lead to reduction in maintenance costs and thus raise productivity a

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39

Kumar, Apurva. "Robust design methodologies : application to compressor blades." Thesis, University of Southampton, 2006. https://eprints.soton.ac.uk/72037/.

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Compressor blades are subtle aerodynamic shapes designed after years of research and insight. They inevitably show deviations from their desired shapes due to manufacturing errors, erosion or foreign object damage. In the present study we focus on seeking compressor blade geometries, that are robust in performance in the presence of geometric uncertainty. Sophisticated tools for representing and propagating uncertainty are employed. Novel method for modeling eroded blade geometry and simulating manufacturing variations with process capability data are presented. These are combined with an auto

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40

Valero, Ricart Omar Ruben. "Multidisciplinary concurrent optimization of gas turbine blades." Thesis, University of Oxford, 2015. https://ora.ox.ac.uk/objects/uuid:b89d8f80-9134-4856-8223-5f55967c0bde.

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This thesis presents the study and development of optimization methods that can perform concurrent aerodynamic-aeroelastic blade optimization in a multi-bladerow environment, and for realistic turbomachinery blade geometries. The Nonlinear Harmonic Phase Solution Method has been chosen as the flow solution method of this work because of its capability to calculate the aeroelasticity features of interest (blade flutter) and the main flow aerodynamic performance in steady flow timescales. The first optimization method that is shown is a more generic non-gradient method with an improved version o

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41

Taylor, John. "The dynamics and stresses of bandsaw blades." Thesis, University of British Columbia, 1986. http://hdl.handle.net/2429/26333.

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This study investigates the stresses and dynamics of stationary, idling and cutting bandsaw blades. A method of obtaining an estimate of the stresses in an idling bandsaw blade is presented. The estimate is determined by measuring the stresses that occur when the blade vibrates in its lowest fundamental modes and assuming that the idling behaviour can be represented by a summation of these modes. The natural frequencies of the bandsaw blade have been measured for various operating conditions and the measured results are compared to existing analytical predictions. A modification to the analys

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42

Ahuja, Anil. "Random vibrations of mistuned periodic structures." Thesis, This resource online, 1990. http://scholar.lib.vt.edu/theses/available/etd-11012008-063055/.

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43

Ozbay, Serkan. "Extension-Twist Coupling Optimization in Composite Rotor Blades." Diss., Georgia Institute of Technology, 2005. http://hdl.handle.net/1853/10422.

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For optimal rotor performance in a tiltrotor aircraft the difference in the inflow and the rotor speeds between the hover and cruise flight modes suggests different blade twist and chord distributions. The blade twist rates in current tiltrotor applications are defined based upon a compromise between the figure of merit in hover and propeller efficiency in airplane mode. However, when each operation mode is considered separately the optimum blade distributions are found to be considerably different. Passive blade twist control, which uses the inherent variation in centrifugal forces on a rot

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44

Pawar, Prashant M. "Structural Health Monitoring Of Composite Helicopter Rotor Blades." Thesis, Indian Institute of Science, 2006. http://hdl.handle.net/2005/273.

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Helicopter rotor system operates in a highly dynamic and unsteady aerodynamic environment leading to severe vibratory loads on the rotor system. Repeated exposure to these severe loading conditions can induce damage in the composite rotor blade which may lead to a catastrophic failure. Therefore, an interest in the structural health monitoring (SHM) of the composite rotor blades has grown markedly in recent years. Two important issues are addressed in this thesis; (1) structural modeling and aeroelastic analysis of the damaged rotor blade and (2) development of a model based rotor health monit

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45

Husain, Al-taie Arkan Khilkhal. "Experimental Study of Radiation From Coated Turbine blades." Thesis, Cranfield University, 1990. http://dspace.lib.cranfield.ac.uk/handle/1826/4553.

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The specific power (or specific thrust) of modern gas turbines is much influenced by the gas temperature at turbine inlet. Even with the use of the best superalloy available and the most advanced cooling configurations, there are competitive pressures to operate engines at even higher gas temperatures. Ceramic coatings operate as thermal barriers and can allow the gas temperature to be increased by 50 to 220 K over the operating gas temperature for an uncoated turbine . It is important that the surface temperature of the blade be determined as accurately as possible. Large uncertainties as to

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46

Nichols, James Franklin. "Two-dimensional analysis of turbine blades and nozzles." Thesis, Georgia Institute of Technology, 2001. http://hdl.handle.net/1853/17673.

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47

Hultman, Hugo. "Validation of Forced Response Methods for Turbine Blades." Thesis, KTH, Kraft- och värmeteknologi, 2015. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-172144.

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48

Khan, Sameer. "Probalistic Stress Rupture Life Analysis of Turbine Blades." Honors in the Major Thesis, University of Central Florida, 2006. http://digital.library.ucf.edu/cdm/ref/collection/ETH/id/970.

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This item is only available in print in the UCF Libraries. If this is your Honors Thesis, you can help us make it available online for use by researchers around the world by following the instructions on the distribution consent form at http://library.ucf.edu/Systems/DigitalInitiatives/DigitalCollections/InternetDistributionConsentAgreementForm.pdf You may also contact the project coordinator, Kerri Bottorff, at kerri.bottorff@ucf.edu for more information.<br>Bachelors<br>Engineering and Computer Science<br>Mechanical Engineering

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Wylie, Dave. "Factoring Blades and Versors in Euclidean Clifford Algebras." Thesis, Southern Illinois University at Edwardsville, 2014. http://pqdtopen.proquest.com/#viewpdf?dispub=1564083.

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<p> This thesis examines different methods of factoring elements of Clifford Algebras, specifically, <i>C</i>&ell;<sub>n,0</sub>. Blades are factored using Fontijne's algorithm and other techniques. Versors are factored using Perwass's algorithm. Writing an element as a sum of blades, which are then factored, can make it more efficient to store or transmit that element. To evaluate the usefulness of expressing a given element of <i>C</i>&ell;<sub> n,0</sub> this way, the number of scalars required to express that element is compared between factored and expanded forms.</p>

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Moffatt, Stuart. "Forced response prediction for industrial gas turbine blades." Thesis, Durham University, 2006. http://etheses.dur.ac.uk/2692/.

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A highly efficient aeromechanical forced response system is developed for predicting resonant forced vibration of turbomachinery blades with the capabilities of fully 3-D non-linear unsteady aerodynamics, 3-D finite element modal analysis and blade root friction modelling. The complete analysis is performed in the frequency domain using the non linear harmonic method, giving reliable predictions in a fast turnaround time. A robust CFD-FE mesh interface has been produced to cope with differences in mesh geometries, and high mode shape gradients. A new energy method is presented, offering an alt

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