Academic literature on the topic 'Linear load'

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Journal articles on the topic "Linear load"

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Khristiana, Harrij Mukti, Sudjito Soeparman, Slamet Wahyudi, and Rini Nur Hasanah. "Analysis of loss on single-phase dry transformers with non-linear load." Eastern-European Journal of Enterprise Technologies 5, no. 8 (113) (2021): 17–22. http://dx.doi.org/10.15587/1729-4061.2021.240233.

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The paper studies power losses in transformers due to non-linear loads. The research aims to analyze the power loss in a single-phase dry transformer under a non-linear load. The research uses an SW43W Power supply type, FlukeView Power Quality Analyzer as a DC or AC power supply on the primary side of the transformer. The non-linear load is connected to the secondary side. The loading test of the dry transformer was carried out at non-linear loads. The load variations used 0 %; 12.5 %; 25 %; 37.5 %; 50 %; 62.5 %; 75 %; 87.5 % and 100 %, as well as variations in the THD value by adjusting the ignition angle (α). The non-linear loads used are Half-Wave Rectifier and Controlled Half-Wave Rectifier with resistive loads with variations in THD values. The results showed that the transformer losses comprised Pno load and Pload. The operation of the transformer with constant input voltage and frequency with THDv<5 % resulted in a constant Pno load value at all load values. The greater the percentage of the load, the higher the load. The increase in THD because of non-linear load will increase the load on the transformer. The value of the derating factor is obtained by connecting the increase in losses (∆PLosses), which is influenced by THD and the increase in temperature T(°C) in dry transformers. When the transformer is loaded with a non-linear load, the derating factor<1. THD and derating factor form a linear relationship, when THD increases, the derating factor value decreases. Linear load on the transformer causes a decrease in its capacity, but if it gets a non-linear load with THD=39.1 %, it can withstand a load of 84.294 %, besides the increase in total harmonic distortion will increase losses and reduce transformer capacity
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Harrij, Mukti Khristiana, Soeparman Sudjito, Wahyudi Slamet, and Nur Hasanah Rini. "Analysis of loss on single-phase dry transformers with non-linear load." Eastern-European Journal of Enterprise Technologies 5, no. 8 (113) (2021): 17–22. https://doi.org/10.15587/1729-4061.2021.240233.

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The paper studies power losses in transformers due to non-linear loads. The research aims to analyze the power loss in a single-phase dry transformer under a non-linear load. The research uses an SW43W Power supply type, FlukeView Power Quality Analyzer as a DC or AC power supply on the primary side of the transformer. The non-linear load is connected to the secondary side. The loading test of the dry transformer was carried out at non-linear loads. The load variations used 0&nbsp;%; 12.5&nbsp;%; 25&nbsp;%; 37.5&nbsp;%; 50&nbsp;%; 62.5&nbsp;%; 75&nbsp;%; 87.5&nbsp;% and 100&nbsp;%, as well as variations in the THD value by adjusting the ignition angle (&alpha;). The non-linear loads used are Half-Wave Rectifier and Controlled Half-Wave Rectifier with resistive loads with variations in THD values. The results showed that the transformer losses comprised P<sub>no load&nbsp;</sub>and P<sub>load</sub>. The operation of the transformer with constant input voltage and frequency with THDv&lt;5&nbsp;% resulted in a constant P<sub>no load&nbsp;</sub>value at all load values. The greater the percentage of the load, the higher the load. The increase in THD because of non-linear load will increase the load on the transformer. The value of the derating factor is obtained by connecting the increase in losses (∆P<sub>Losses</sub>), which is influenced by THD and the increase in temperature T(&deg;C) in dry transformers. When the transformer is loaded with a non-linear load, the derating factor&lt;1. THD and derating factor form a linear relationship, when THD increases, the derating factor value decreases. Linear load on the transformer causes a decrease in its capacity, but if it gets a non-linear load with THD=39.1&nbsp;%, it can withstand a load of 84.294&nbsp;%, besides the increase in total harmonic distortion will increase losses and reduce transformer capacity
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Mat Saleh, Syadatul Syaeda binti, Nurul Husna Jamian, and Najihan Awang@Ali. "Team Teaching Load using Linear Programming." Journal of Computing Research and Innovation 4, no. 1 (2019): 8–15. http://dx.doi.org/10.24191/jcrinn.v4i1.115.

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Assignment of teaching loads refers to the allocation of teaching hours among academic staff. It will be the ideal way to assign the right courses to the right staff based on their expertise, preference and experience. The common practice in this department to allocate the teaching load is done manually through trial-and-error using Microsoft Excel which is inefficient and time consuming. Moreover, the manual allocation may lead to bias judgement and get unfavourable courses among academic staff. Thus, this study aims to propose a teaching load allocation model which able to optimize the teaching quality. A primary data has been collected using google form among 25 lecturers with 13 courses considered. Then, a linear programming model was applied based on department policies as constraints in order to find an optimal solution. A feasible solution will be solved using LINGO optimization software and the model serves as a best tool to assist head of department to allocate teaching loads. It found that the model proposed is suitable to be employed for teaching load allocation in this department .
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Visweswara Rao, G. "Linear Dynamics of an Elastic Beam Under Moving Loads." Journal of Vibration and Acoustics 122, no. 3 (2000): 281–89. http://dx.doi.org/10.1115/1.1303822.

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The dynamic response of an Euler-Bernoulli beam under moving loads is studied by mode superposition. The inertial effects of the moving load are included in the analysis. The time-dependent equations of motion in modal space are solved by the method of multiple scales. Instability regions of parametric resonance are identified and the moving mass effect is shown to significantly affect the transient response of the beam. Importance of modal interaction arising out of the possible internal resonance is highlighted. While the external resonance is due to the gravity effects of the moving load, the parametric and internal resonance solely depends on the load mass parameter—ratio of the moving load mass to the beam mass. Numerical results show the influence of the load inertia terms on the beam response under either a single moving load or a series of moving loads. [S0739-3717(00)01703-7]
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Bekirova, М. "STABILITY OF RODS WITH INITIAL IMPERFECTIONS IN THE FORM OF ECCENTRICITY OF LOAD APPLICATION UNDER LINEAR AND NON-LINEAR CREEP CONDITIONS." Mechanics And Mathematical Methods 5, no. 1 (2023): 110–20. http://dx.doi.org/10.31650/2618-0650-2023-5-1-110-120.

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Stability of a compressed rod having initial imperfections in the form of eccentricity of applied load under conditions of linear and nonlinear creep is considered. It is noted that all real elements have some initial imperfections in the form of technological deflections, eccentricities of applied loads, etc., so they begin to bulge from the very beginning of loading. Another important factor in stability theory is the consideration of material creep. In this regard, the loading process is divided into two phases: the instantaneous loading process and the creep phase under constant external load. Moreover, creep can be time-limited or unrestricted. In the paper formulas for determination of critical forces of stability loss of the rod having initial imperfections, under short-term and long-term action of load are obtained. The equation allowing to determine time of the first crack appearance is derived. Derived are equations the roots of which are loads at action of which the first cracks appear at initial moment of time and at arbitrarily long period of load action. Analysis of acting force determining the character of rod deformation is executed. From the constructed stability equation it is possible to determine the critical force corresponding to the critical length of the section with cracks. For similar problems in nonlinear formulation formulas for determining critical force and critical displacement corresponding to maximum load are obtained. For the case of long duration load the equation which establishes relationship between load and displacement is obtained. Equation for determination of critical force under prolonged action of load has been derived. It has been established that critical displacement is the same under short- and continuous action of load. It is shown that at any intermediate moment critical displacement can be achieved under load lying in certain interval. Keywords: stability, rod, initial imperfection, eccentricity, linear creep, non-linear creep, critical force, crack, critical displacement.
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Ghaderi, S. F., J. Razmi ., and B. Ostadi . "A Mathematical Model for Load Optimization: Linear Load Curves." Journal of Applied Sciences 6, no. 4 (2006): 883–87. http://dx.doi.org/10.3923/jas.2006.883.887.

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Mastoras, Aristeidis, and Thomas R. Gross. "Load-balancing for load-imbalanced fine-grained linear pipelines." Parallel Computing 85 (July 2019): 178–89. http://dx.doi.org/10.1016/j.parco.2019.01.002.

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Чиркова, Юлия Васильевна, and Julia Chirkova. "Machine load balancing game with linear externalities." Mathematical Game Theory and Applications 13, no. 2 (2021): 62–79. http://dx.doi.org/10.17076/mgta_2021_2_36.

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The Machine Load Balancing Game with linear externalities is considered. A set of jobs is to be assigned to a set of machines with different latencies depending on their own loads and also loads on other machines. Jobs choose machines to minimize their own latencies. The social cost of a schedule is the maximum delay among all machines, i.e. {\it makespan. For the case of two machines in this model an Nash equilibrium existence is proven and of the expression for the Price of Anarchy is obtained.
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Naz, R., and F. M. Mahomed. "Dynamic Euler-Bernoulli Beam Equation: Classification and Reductions." Mathematical Problems in Engineering 2015 (2015): 1–7. http://dx.doi.org/10.1155/2015/520491.

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We study a dynamic fourth-order Euler-Bernoulli partial differential equation having a constant elastic modulus and area moment of inertia, a variable lineal mass densityg(x), and the applied load denoted byf(u), a function of transverse displacementu(t,x). The complete Lie group classification is obtained for different forms of the variable lineal mass densityg(x)and applied loadf(u). The equivalence transformations are constructed to simplify the determining equations for the symmetries. The principal algebra is one-dimensional and it extends to two- and three-dimensional algebras for an arbitrary applied load, general power-law, exponential, and log type of applied loads for different forms ofg(x). For the linear applied load case, we obtain an infinite-dimensional Lie algebra. We recover the Lie symmetry classification results discussed in the literature wheng(x)is constant with variable applied loadf(u). For the general power-law and exponential case the group invariant solutions are derived. The similarity transformations reduce the fourth-order partial differential equation to a fourth-order ordinary differential equation. For the power-law applied load case a compatible initial-boundary value problem for the clamped and free end beam cases is formulated. We deduce the fourth-order ordinary differential equation with appropriate initial and boundary conditions.
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Sharma, Akhilesh. "Open-Loop Voltage Control Voltage Source Inverter for a Linear Load & Non-Linear Load." Journal of Electrical and Electronic Engineering 3, no. 1 (2015): 13. http://dx.doi.org/10.11648/j.jeee.s.2015030101.12.

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Dissertations / Theses on the topic "Linear load"

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Van, der Merwe Wim. "PWM converter for a highly non-linear plasma load." Thesis, Stellenbosch : University of Stellenbosch, 2005. http://hdl.handle.net/10019.1/3025.

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Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2005.<br>This thesis discuss an investigation into the applicability of modern high frequency power conversion technology in the plasma mineral processing industry. The physics governing the plasma in a processing environment are analysed to provide a clear understanding of this plasma as electrical load. This was done to create an electrical model for the plasma as load and gain understanding into the electrical supply requirements. Modern high frequency power conversion technology is contrasted with thyristor controlled line frequency technologies to provide a suitable starting point for the study. A 3 kW soft switched converter is proposed for application with a plasma load. This converter is designed and verified. The small-signal signature of the proposed converter under peak current mode control is investigated and a new model is proposed to describe this control configuration.
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POMA, CARLOS ENRIQUE PORTUGAL. "AN ITERATIVE SOLVER FOR LINEAR-SYSTEMS: APPLICATION IN LOAD FLOW." PONTIFÍCIA UNIVERSIDADE CATÓLICA DO RIO DE JANEIRO, 2010. http://www.maxwell.vrac.puc-rio.br/Busca_etds.php?strSecao=resultado&nrSeq=17554@1.

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COORDENAÇÃO DE APERFEIÇOAMENTO DO PESSOAL DE ENSINO SUPERIOR<br>Este trabalho desenvolve um solucionador iterativo baseado no método Resíduo Mínimo Generalizado (GMRES) para solucionar o subproblema linear do problema de fluxo de carga, com destaque para cenários de difícil convergência. O solucionador agrega uma estratégia de reordenamento para minimização do número total de novos elementos não-nulos e um pré-condicionador baseado no algoritmo de Doolittle, com regra de preenchimento de elementos não-nulos baseada no erro resultante. O solucionador foi implementado em um programa computacional de fluxo de carga, a fim de se verificar sua robustez e eficiência em diversos sistemas-teste e diferentes condições de operação. Também é proposto um método para o ajuste dos parâmetros dos solucionadores iterativos, que permite identificar intervalos de valores permissíveis para cada um dos parâmetros, identificando os mais adequados, visando garantir a robustez e melhorar o desempenho do solucionador.<br>This work develops an iterative solver based on Generalized Minimal Residual method (GMRES) to solve the load flow linear subproblem, especially in scenarios of difficult convergence. The solver combines a reordering strategy to minimise the total number of fill-in terms and a preconditioning strategy based on the Doolittle algorithm with a fill-in dropping strategy based on the resulting error. The solver was implemented into a computational load flow program in order to verify its robustness and efficiency in several test-systems and different operating conditions. It is also proposed a method for adjusting the iterative solver parameters, the method is able to identify intervals of permissible values for each parameter, identifying the most appropriate in order to ensure the robustness and improve the solver performance.
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Rögnvaldsson, Kristján Óttar. "Multi-Objective Mixed-Integer Linear Optimisation of Aircraft Load Planning." Thesis, KTH, Optimeringslära och systemteori, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-253363.

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A general multi-objective optimisation model is developed for the load planning decision process of a bulk loaded commercial aircraft, using the Airbus A321 fitted with additional fuel tanks as a baseline platform. The model’s input is a specific set of load items, with associated quantities, mass and volume. The output is a load plan, stating where each item should be loaded and in what quantity. The load plans should be optimal with respect to a target centre of gravity range and handling efficiency. Furthermore, the solutions should be robust with respect to perturbations in the input data. Three objective functions and a set of constraints are defined to achieve this task. A constraint that ensures the ground stability of the aircraft is developed and analysed. A lexicographic approach is used solve the multi-objective problem, by sequentially solving a set of mixed-integer linear programs. The sequence is determined from a priority ranking of the objectives. Testing is carried out with data from an operator of the A321, with four different test cases. Test results indicate that the model is capable of solving the load planning problem for the baseline aircraft. The centre of gravity values are within the optimal range, and the load distributions are efficient. Additional margins on aircraft limits assist with maintaining feasibility in case of input perturbation. The model is also robust with respect to the highly variable test data. The main causes of infeasibility are mixing constraints and additional balance envelope margins. The ground stability constraint does not cause any significant amount of infeasibilities, and primarily increases the safety level of the load plans. A strength of the model is its relatively simple handling of the multiple objectives, and the small number of tunable parameters also makes the model controllable. A trained agent in the industry is able to understand and control the model without an extensive technical background. The test process used differs slightly from the actual industry load planning process. As a result, testing only allows for evaluation of the model’s ability to solve the load planning problem, and gives no justification for implementation in real-world operations. Such an evaluation requires a prototype to be tested in an operational environment using the actual process. As testing was only done for the baseline aircraft, with one set of test data and model parameters, a justifiable conclusion cannot be reached on the model’s applicability to other bulk loaded aircraft. Therefore, it is recommended to carry out further testing on different aircraft as the next step in them model’s evaluation. iv<br>En allmänn flermåls optimeringsmodell utvecklas för besluttsprocessen relaterat till lastning av ett kommersiellt flygplan, som använder Airbus A321 utrustad med ytterligare bränslestankar som en bas. Modellens indata är ett specifikt set av artiklar som ska lastas tillsammans med information om mängd, tyngd och volym. Utvärdet är en beskrivande plan som visar var varje artikel ska lastas och i vilken mängd. Planen ska vara optimal med hänsyn till ett specifikt tyngdpunkts intervall och vara effectiv för lastningsoperationer. Dessutom ska den vara robust med hänsyn till störningar i indatan. Tre målfunktioner tillsammans med ett set av begränsningar används för att lösa problemet. En specifik begränsning som säkrar flygplanets stabilitet på grunden utvecklas och dess känslighet analyseras. En lexikografisk metod används för att lösa flermåls problemet, där lösar en sekvens av blandade heltalsprogrammer. Sekvensen är definierad ut från en prioritetsordning av de olika målfunktioner. Testning av modellen är utförd med indata från en operatör av A321 basflygplanet med fyra olika testfall. Testresultaten visar att modellen kan användas för att lösa lastningsproblemet för basflygplanet. Tyngdpunktsvärden är inom det optimal intervall och fördelningen av artiklar är effektiv. Extra marginaler på flygplansbegränsningar hjälper med att säkra lösningen under störningar på indatan. Modellen är också robust med hänsyn till högvarierad indata. Huvudorsaker till omöjliga testfall, de utan lösningar, är begränsningar på blandning av artiklar samt extra marginaler på flygplansbegränsningar. Begränsningen för grund stabilitet är inte en orsak till omöjlighet, och ökar primärt säkerhetsnivån på lösningen. En styrka till modellen är dess enkel hantering av de olika målfunktioner och de få parametrar gör modellen kontrollbar. En utbildad agent från industrin kan förstå och kontrollera modellen, utan att ha en teknisk bakgrund. Testprocessen som används representerar inte exakt industriprocessen. Testprocessen kan därför bara användas till att utvärdera modellens förmåga till att lösa lastningsproblemet, och ger ingen motivering på bruk i verkliga operationer. En utvärdering på den förmåga krävs en utveckling av en prototyp i verkliga världen. Testning av bara en typ av basflygplan, tillsammans med ett set av indata och modellparametrar, ger inte en grund till en konklusion på modellens tillämplighet för andra flygplan. Därför rekommenderas det att utföra ytterligare testning på andra flygplan som nästa steg i modellens utvärdering.
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Chaikittiratana, Arisara. "Non-linear viscoelastic strain analysis for engineering polymers." Thesis, University of Oxford, 2000. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.342239.

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Pieraccini, Luca. "Shear behaviour of reinforced cconcrete slab under concentrated load: an investigation through non-linear and sequentially linear analysis." Master's thesis, Alma Mater Studiorum - Università di Bologna, 2013. http://amslaurea.unibo.it/5902/.

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English: The assessment of safety in existing bridges and viaducts led the Ministry of Public Works of the Netherlands to finance a specific campaing aimed at the study of the response of the elements of these infrastructures. Therefore, this activity is focused on the investigation of the behaviour of reinforced concrete slabs under concentrated loads, adopting finite element modeling and comparison with experimental results. These elements are characterized by shear behaviour and crisi, whose modeling is, from a computational point of view, a hard challeng, due to the brittle behavior combined with three-dimensional effects. The numerical modeling of the failure is studied through Sequentially Linear Analysis (SLA), an alternative Finite Element method, with respect to traditional incremental and iterative approaches. The comparison between the two different numerical techniques represents one of the first works and comparisons in a three-dimensional environment. It's carried out adopting one of the experimental test executed on reinforced concrete slabs as well. The advantage of the SLA is to avoid the well known problems of convergence of typical non-linear analysis, by directly specifying a damage increment, in terms of reduction of stiffness and resistance in particular finite element, instead of load or displacement increasing on the whole structure . For the first time, particular attention has been paid to specific aspects of the slabs, like an accurate constraints modeling and sensitivity of the solution with respect to the mesh density. This detailed analysis with respect to the main parameters proofed a strong influence of the tensile fracture energy, mesh density and chosen model on the solution in terms of force-displacement diagram, distribution of the crack patterns and shear failure mode. The SLA showed a great potential, but it requires a further developments for what regards two aspects of modeling: load conditions (constant and proportional loads) and softening behaviour of brittle materials (like concrete) in the three-dimensional field, in order to widen its horizons in these new contexts of study.
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Jiao, Yaguang. "Non-linear load-deflection models for seafloor interaction with steel catenary risers." Thesis, [College Station, Tex. : Texas A&M University, 2007. http://hdl.handle.net/1969.1/ETD-TAMU-1279.

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Elsayed, Ahmed L. "A new approach for non-linear load-settlement assessment of shallow foundations." abstract and full text PDF (free order & download UNR users only), 2008. http://0-gateway.proquest.com.innopac.library.unr.edu/openurl?url_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:dissertation&res_dat=xri:pqdiss&rft_dat=xri:pqdiss:1453588.

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Brazas, Michael L. "Cognitive load theory and programmed instruction." [Tampa, Fla.] : University of South Florida, 2005. http://purl.fcla.edu/fcla/etd/SFE0001011.

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Siveski, Zlatan. "Non-linear structural analysis of shear connected cavity walls subject to wind load." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 1997. http://www.collectionscanada.ca/obj/s4/f2/dsk2/ftp04/mq23496.pdf.

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Tola, Adrian Patricio. "Development of a Comprehensive Linear Response History Analysis Procedure for Seismic Load Analysis." Thesis, Virginia Tech, 2010. http://hdl.handle.net/10919/36106.

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This thesis reviews the parameters required to perform linear response history analysis according to Chapter 16 of the American Standard ASCE 7-10. A careful analysis is presented about the selection of ground motions using real records and using artificial records generated such that their response spectrum matches with a defined target spectrum; three different techniques are studied for the generation of these artificial records. Also, this document revises the scaling of ground motion techniques in the American Standard ASCE-7 as well as in other seismic codes. It presents a detailed analysis of the variables influencing the scaling of ground motions, and it suggests a new scaling technique for linear response history analysis. The assumptions made establishing the flexibility of the diaphragms are also analyzed as well as dynamic methods to include accidental torsion when doing a linear response history analysis. Other modeling issues such as the orientation of the ground motion axis, scaling of element forces and displacements, orthogonal loading, solution techniques, P-Delta effects, modeling of the basement, and calculation of drifts are also studied in the context of linear response history analysis. The thesis concludes with suggested code language for linear response history analysis intended to be considered in future editions of the American Standard ASCE 7.<br>Master of Science
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Books on the topic "Linear load"

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Center, Lewis Research, ed. Analog synthesized fast-variable linear load. Sverdrup Technology, Inc., Lewis Research Center Group, 1991.

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Center, Lewis Research, ed. Analog synthesized fast-variable linear load. Sverdrup Technology, Inc., Lewis Research Center Group, 1991.

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Jensen, Jørgen Juncher. Non-linear wave load predictions for marine structures. Danmarks tekniske universitet, 1994.

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Serbousek, M. O. Linear load-transfer mechanics of full-grouted roof bolts. U.S. Dept. of the Interior, Bureau of Mines, 1987.

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Christen, Peter. A parallel iterative linear system solver with dynamic load balancing. Shaker, 1999.

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Murthy, V. R. Linear and nonlinear dynamic analysis of redundant load path bearingless rotor systems. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1994.

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S, Rauch Jeffrey, and United States. National Aeronautics and Space Administration., eds. Controllability of free-piston Stirling engine/linear alternator driving a dynamic load. National Aeronautics and Space Administration, 1993.

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Center, Ames Research, ed. Linear and nonlinear dynamic analysis of redundant load path bearingless rotor systems. National Aeronautics and Space Administration, Ames Research Center, 1985.

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S, Rauch Jeffrey, Santiago Walter, and United States. National Aeronautics and Space Administration., eds. Dynamic analysis of free-piston Sterling engine/linear alternator-load system-experimentally validated. National Aeronautics and Space Administration, 1992.

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Center, NASA Glenn Research, ed. A 3-D magnetic analysis of a Stirling convertor linear alternator under load. National Aeronautics and Space Administration, Glenn Research Center, 2001.

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Book chapters on the topic "Linear load"

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Rychlik, Igor, Sayan Gupta, and Georg Lindgren. "Non-Linear Load Transformations." In Fatigue Prediction for Random Loads. CRC Press, 2025. https://doi.org/10.1201/9781003019947-10.

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Rust, Wilhelm. "Load Incrementation in a Non-linear Analysis." In Non-Linear Finite Element Analysis in Structural Mechanics. Springer International Publishing, 2014. http://dx.doi.org/10.1007/978-3-319-13380-5_4.

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Stirb, Adelin, Adrian Ciutina, Andrei Forton, Ciprian Costescu, and Paul Marc. "Analysis of the Pavement Response with Total/Partial Link Between Layers to the Action of Traffic Load." In Lecture Notes in Civil Engineering. Springer Nature Switzerland, 2024. http://dx.doi.org/10.1007/978-3-031-57800-7_6.

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AbstractThe paper investigates the response of the pavement of a road sector analyzed to the traffic load that was determined numerically by using Abaqus numerical modelling software. This tool offers advanced analysis options in comparison with the normative road structure dimensioning tool. Thus, in contrast to the current use road structure dimensioning program, the FEM software allows the definition of the interfaces between layers and switch loads from static load to moving load, based on the determination of the resilient stresses and deformations in road structures by using the classical linear elastic multilayer model. The aim of this study was to determine whether the road pavement with deficiencies of adhesion between asphalt layers can take over the calculated traffic load considered in the study, or the proportion of design traffic load that can be taken over. That would allow an assessment of the service operation life of the road pavement and, implicitly, of the possibility of its yielding before the end of the perspective period considered.
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Chirkova, Julia V. "Maximizing the Minimum Processor Load with Linear Externalities." In Communications in Computer and Information Science. Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-86433-0_10.

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Oozeer, Muhammad Yasser, and Rajeshree Ramjug-Ballgobin. "Optimization of Load Frequency Control for Non-linear System." In Smart and Sustainable Engineering for Next Generation Applications. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-18240-3_4.

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Cammarano, A., A. Gonzalez-Buelga, S. A. Neild, D. J. Wagg, S. G. Burrow, and D. J. Inman. "Optimum Load for Energy Harvesting with Non-linear Oscillators." In Special Topics in Structural Dynamics, Volume 6. Springer New York, 2013. http://dx.doi.org/10.1007/978-1-4614-6546-1_58.

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Xu, Song-Jin, Zhi-ping Tang, Wen Wu, Hua Zhang, Ya-qun Liu, and Qihua Zhang. "Non-linear Analyses on Pile-soil Load Transfer Behavior." In Physical Modelling in Geotechnics. Routledge, 2022. http://dx.doi.org/10.1201/9780203743362-120.

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Manalathody, Abhishek, Kishoor Santhana Krishnan, Jisnu Adindtra Subramanian, Sakthivel Thangavel, and Rajesh Senthil Kumar Thangeswaran. "Non-linear Controller for a Drone with Slung Load." In Recent Advances in Aerospace Engineering. Springer Nature Singapore, 2024. http://dx.doi.org/10.1007/978-981-97-1306-6_18.

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Liu, Xuecheng, Chuangeng Tian, and Lei Chen. "Load-Balanced Delivery Strategy for Linear Wireless Sensor Networks." In Simulation Tools and Techniques. Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-72792-5_57.

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Yao, Fulai, and Yaming Yao. "Most Commonly Used Actuator–Motor." In Efficient Energy-Saving Control and Optimization for Multi-Unit Systems. Springer Nature Singapore, 2024. http://dx.doi.org/10.1007/978-981-97-4492-3_6.

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AbstractIn energy-saving control, a large number of electric motors are used for load distribution and devices switching. A lot of rotary motions, linear motion or other forms of mechanical motion are mostly driven by motors. It can be said that motors are the most commonly used actuators in the field of electrical engineering and automation. After being connected to a suitable power supply, the motor generates rotary motion, and the linear motor produce linear motion.
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Conference papers on the topic "Linear load"

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Song, Jiancai, Qianxing Dong, Kangning Wang, and Xiaoyu Gao. "A Time-Frequency Collaborative Linear Model Heat Load Prediction Algorithm." In 2025 IEEE 6th International Seminar on Artificial Intelligence, Networking and Information Technology (AINIT). IEEE, 2025. https://doi.org/10.1109/ainit65432.2025.11035316.

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Garg, Raghav, Amit Mittal, Karimulla Syed, Mohammed Asim, Abhishek Chakravorty, and Shweta Goyal. "Linear Quadratic Regulator (LQR)-Based Load Frequency Control in Power Systems." In 2024 2nd World Conference on Communication & Computing (WCONF). IEEE, 2024. http://dx.doi.org/10.1109/wconf61366.2024.10692249.

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Barnawal, Prakash Ji, and S. M. Tripathi. "Non-linear load compensation using STATCOM." In 2016 International Conference on Emerging Trends in Electrical Electronics & Sustainable Energy Systems (ICETEESES). IEEE, 2016. http://dx.doi.org/10.1109/iceteeses.2016.7581375.

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Ruehli, Albert E., and Jerry Hayes. "Nonlinear circuit solver with linear interconnect load." In 2008 IEEE 17th Conference on Electrical Performance of Electronic Packaging (EPEP). IEEE, 2008. http://dx.doi.org/10.1109/epep.2008.4675912.

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de Vasconcellos, Arnulfo Barroso, Gabriela Nunes Lopes, Etiane Oliveira Ponciano De Carvalho, Fabricio Parra Santilio, Priscila Costa Nascimento, and Teresa Irene Ribeiro de Carvalho Malheiro. "The reactive energy compensation of linear loads using a switched electronic load." In 2018 Simposio Brasileiro de Sistemas Eletricos (SBSE) [VII Brazilian Electrical Systems Symposium (SBSE)]. IEEE, 2018. http://dx.doi.org/10.1109/sbse.2018.8395536.

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Jereminov, Marko, Amritanshu Pandey, Hyun Ah Song, Bryan Hooi, Christos Faloutsos, and Larry Pileggi. "Linear load model for robust power system analysis." In 2017 IEEE PES Innovative Smart Grid Technologies Conference Europe (ISGT-Europe). IEEE, 2017. http://dx.doi.org/10.1109/isgteurope.2017.8260315.

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Vollmer, Frank, and Hubertus Murrenhoff. "Hydraulic Linear Actuators with High Dynamic Load Stiffness." In International Off-Highway & Powerplant Congress. SAE International, 2002. http://dx.doi.org/10.4271/2002-01-1496.

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Ouyang Lin, Qi Jingjing, Zhou Qin, and Pu Qiumei. "A New Linear Programming Based Load-Shedding Strategy." In 2012 11th International Symposium on Distributed Computing and Applications to Business, Engineering & Science. IEEE, 2012. http://dx.doi.org/10.1109/dcabes.2012.31.

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Dominguez, E., P. Yorio, E. Ferrigno, J. L. Piña, and M. Somoza. "Downhole Linear Reducer Application for Rod Load Optimization." In SPE Latin America and Caribbean Petroleum Engineering Conference. Society of Petroleum Engineers, 2017. http://dx.doi.org/10.2118/185475-ms.

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Costa, Analiza Dalla, Bibiana P. Ferraz, Mariana Resener, and Sergio Haffner. "Linear Load Flow Formulation for Unbalanced Distribution Systems." In 2019 IEEE PES Innovative Smart Grid Technologies Conference - Latin America (ISGT Latin America). IEEE, 2019. http://dx.doi.org/10.1109/isgt-la.2019.8895503.

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Reports on the topic "Linear load"

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Niedra, J. M. Analog synthesized fast-variable linear load. Office of Scientific and Technical Information (OSTI), 1991. http://dx.doi.org/10.2172/10181566.

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Horgan, Cornelius O. Load Diffusion in Linear and Nonlinear Solid Mechanics. Defense Technical Information Center, 2001. http://dx.doi.org/10.21236/ada398141.

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Dinda, Peter A., and David R. O'Hallaron. An Evaluation of Linear Models for Host Load Prediction. Defense Technical Information Center, 1998. http://dx.doi.org/10.21236/ada358577.

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Lifflander, Jonathan, Pierre Pebay, Sean McGovern, and Nicole Slattengren. Modeling Workloads of a Linear Electromagnetic Code for Load Balancing Matrix Assembly. Office of Scientific and Technical Information (OSTI), 2023. http://dx.doi.org/10.2172/2430181.

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Crozier, Jonathan. The neutronic impact of a variable-diameter Li-6 linear load on fuel-lattice power distributions and TPBAR rodworth. Office of Scientific and Technical Information (OSTI), 2019. http://dx.doi.org/10.2172/1645019.

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Riveros, Guillermo, Felipe Acosta, Reena Patel, and Wayne Hodo. Computational mechanics of the paddlefish rostrum. Engineer Research and Development Center (U.S.), 2021. http://dx.doi.org/10.21079/11681/41860.

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Purpose – The rostrum of a paddlefish provides hydrodynamic stability during feeding process in addition to detect the food using receptors that are randomly distributed in the rostrum. The exterior tissue of the rostrum covers the cartilage that surrounds the bones forming interlocking star shaped bones. Design/methodology/approach – The aim of this work is to assess the mechanical behavior of four finite element models varying the type of formulation as follows: linear-reduced integration, linear-full integration, quadratic-reduced integration and quadratic-full integration. Also presented is the load transfer mechanisms of the bone structure of the rostrum. Findings – Conclusions are based on comparison among the four models. There is no significant difference between integration orders for similar type of elements. Quadratic-reduced integration formulation resulted in lower structural stiffness compared with linear formulation as seen by higher displacements and stresses than using linearly formulated elements. It is concluded that second-order elements with reduced integration and can model accurately stress concentrations and distributions without over stiffening their general response. Originality/value – The use of advanced computational mechanics techniques to analyze the complex geometry and components of the paddlefish rostrum provides a viable avenue to gain fundamental understanding of the proper finite element formulation needed to successfully obtain the system behavior and hot spot locations.
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Chauhan. L52134 Development of Methods For Assessing Corrosion Metal Loss Defects In Casing Strings. Pipeline Research Council International, Inc. (PRCI), 2003. http://dx.doi.org/10.55274/r0010892.

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An industry survey, dominated by PRCI member companies, was undertaken to gather key information regarding the design, operation and inspection of well bore casing strings. The aim of the survey was to gather information regarding the design standards, fields, gas composition, completion configuration, operational details, inspection methods and type of damage found. Survey results representing 67 storage facilities with a total of 4724 wells were received. This represents approximately 16% of US gas storage facilities. Facilities with initial completion dates between 1920 and 1990 were represented within the survey. The date of conversion from production to gas storage of the responding facilities ranged from the 1920�s to 2000. Non-linear finite element analysis has been used to determine the significance of an isolated pit corrosion metal loss defect in tubing/casing strings subject to the bounding load cases. Pit defects of depths up to 80% of the wall thickness (t) and diameter 2t were investigated to determine the failure behavior under the nineteen bounding load cases. Nine full-scale burst tests were undertaken in order to determine whether existing assessment methods could be used to predict failure of casing and tubing. Failure loci of 2t diameter and 80% deep defects have been derived for casing subject to combined loading. Full scale testing has only been undertaken with internal pressure loading to validate the approach taken to predict failure.
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Allen, Luke, Joon Lim, Robert Haehnel, and Ian Detwiller. Rotor blade design framework for airfoil shape optimization with performance considerations. Engineer Research and Development Center (U.S.), 2021. http://dx.doi.org/10.21079/11681/41037.

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A framework for optimizing rotor blade airfoil shape is presented. The framework uses two digital workflows created within the Galaxy Simulation Builder (GSB) software package. The first is a workflow enabling the automated creation of a surrogate model for predicting airfoil performance coefficients. An accurate surrogate model for the rapid generation of airfoil coefficient tables has been developed using linear interpolation techniques that is based on C81Gen and ARC2D CFD codes. The second workflow defines the rotor blade optimization problem using GSB and the Dakota numerical optimization library. The presented example uses a quasi-Newton optimization algorithm to optimize the tip region of the UH-60A main rotor blade with respect to vehicle performance. This is accomplished by morphing the blade tip airfoil shape for optimum power, subject to a constraint on the maximum pitch link load.
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Andrawes, Bassem, and Dachina Gunasekaran. Testing, Analysis, and Load Rating of Precast Prestressed Concrete Deck Beams with Transverse Cracks. Illinois Center for Transportation, 2025. https://doi.org/10.36501/0197-9191/25-002.

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This study focused on understanding the impact of transverse cracks on the residual capacity and load rating analysis of in-service precast prestressed concrete (PPC) deck beams. Two decommissioned (33 × 36 and 21 × 36) PPC deck beams were tested under four-point bending loads to assess the impact of transverse cracks on the structural performance of the beams. Finite element and theoretical cracked section analyses were also performed to investigate the capacity of the as-built and cracked PPC deck beam. Transverse cracks reduced the load rating capacity of the 33 × 36 beam by almost 34%, which subsequently reduced the capacity-based load rating factor by 22% under the HS-20 truck load. The experimental investigation of the 21 × 36 PPC deck beam showed that the load required to induce visible cracks in the beam was 95.5% of its AASHTO live load capacity. The load rating of the cracked 21 × 36 beam was 73.6% lower than its as-built capacity, exhibiting a severe reduction in its load-bearing capacity. A parametric study was conducted to understand the effect of the influencing parameters, like the beam geometry and material properties, on the damaged beams’ behavior. For PPC deck beams with rectangular voids, the statistically significant parameters were span length, strand diameter, and skew angle. In the parametric study, the inventory load rating factor of the prestressing strands in tension was predicted to decrease linearly for a crack width up to 0.64 mm, while the capacity inventory rating factor was predicted to decrease up to 73.8% for a crack width of 0.64 mm.
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Eberlein, Robert, and Sven Düzel. Fatigue lifetime analysis of POM gears for generalized tooth root shapes. Universidad de los Andes, 2024. https://doi.org/10.51573/andes.pps39.gs.ms.1.

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The current calculation methods for determining the tooth root load capacity of polymer gears (e.g., VDI 2736) are based on the same assumptions as those for steel gears. However, due to the non-linear material behavior, temperature, and rate dependency of polymers, these predictions are often inaccurate. A previous study employed rate-dependent nonlinear viscoplastic finite element (FE) modelling of polyoxymethylene (POM) to quantify material influences not considered in standard metal gear assumptions. A lifetime model was developed and validated to predict tooth root fracture based on rotational speed for a constant tooth root geometry. In this study, the existing damage model is adapted and validated to include the dependency on notch (tooth root) geometry. The extension of the model to two damage parameters allows for a geometry-independent representation of the nonlinear speed dependency of tooth root breakage. This correlative modelling approach incorporates two independent damage mechanisms inside the material which lead to tooth root breakage failure of the gear. To map these mechanisms, local material states at the crack initiation point are used as damage parameters. Calibration of the bi-parametric damage model with experimental data shows that model predictions fall within the experimental scatter. Further research is ongoing to extend the damage model regarding generalized torque loading conditions.
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