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Bibliografias temáticas / Simplified methods

Literatura científica selecionada sobre o tema "Simplified methods"

Autor: Grafiati

Publicado: 24 de novembro de 2022

Última modificação: 24 de janeiro de 2024

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Artigos de revistas
Teses / dissertações
Livros
Capítulos de livros
Trabalhos de conferências
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Artigos de revistas sobre o assunto "Simplified methods":

1

El-Ghezawi, Omar Moh’d El-Basheer. "Simplified Methods for Eigenvalue Assignment". Advances in Pure Mathematics 05, n.º 07 (2015): 383–89. http://dx.doi.org/10.4236/apm.2015.57037.

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2

Dobry, Ricardo. "Simplified methods in Soil Dynamics". Soil Dynamics and Earthquake Engineering 61-62 (junho de 2014): 246–68. http://dx.doi.org/10.1016/j.soildyn.2014.02.008.

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3

Perraud, Jean, Daniel Arnal, Gregoire Casalis, Jean-Pierre Archambaud e Raffaele Donelli. "Automatic Transition Predictions Using Simplified Methods". AIAA Journal 47, n.º 11 (novembro de 2009): 2676–84. http://dx.doi.org/10.2514/1.42990.

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4

Kuznetsov, Yu K., I. C. Nascimento, R. M. O. Galvão e W. P. De Sá. "Simplified magnetic diagnostic methods for tokamaks". Nuclear Fusion 38, n.º 9 (setembro de 1998): 1385–95. http://dx.doi.org/10.1088/0029-5515/38/9/313.

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5

Davis, S. F. "Simplified Second-Order Godunov-Type Methods". SIAM Journal on Scientific and Statistical Computing 9, n.º 3 (maio de 1988): 445–73. http://dx.doi.org/10.1137/0909030.

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6

Buchanan, G. R., e M. Sallah. "Some simplified methods for infinite elements". Computational Mechanics 6, n.º 3 (1990): 167–72. http://dx.doi.org/10.1007/bf00350233.

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7

Ouellette, Michael J. "Estimation of Measurement Uncertainty: Simplified Methods". NCSLI Measure 2, n.º 3 (setembro de 2007): 56–68. http://dx.doi.org/10.1080/19315775.2007.11721387.

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8

Geraets, Luc H. "Simplified seismic analysis methods in Belgium". Nuclear Engineering and Design 123, n.º 2-3 (outubro de 1990): 299–304. http://dx.doi.org/10.1016/0029-5493(90)90250-2.

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9

Betbeder-Matibet, J., e P. Labbé. "Simplified seismic analysis methods in France". Nuclear Engineering and Design 123, n.º 2-3 (outubro de 1990): 305–12. http://dx.doi.org/10.1016/0029-5493(90)90251-r.

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10

Watabe, M. "Simplified seismic analysis methods in Japan". Nuclear Engineering and Design 123, n.º 2-3 (outubro de 1990): 321–25. http://dx.doi.org/10.1016/0029-5493(90)90253-t.

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Teses / dissertações sobre o assunto "Simplified methods":

1

Aggarwal, Keshav. "Subconvexity Bounds and Simplified Delta Methods". The Ohio State University, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1555064743753817.

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2

OLIVEIRA, MARIA FERNANDA FIGUEIREDO DE. "CONVENTIONAL, HYBRID AND SIMPLIFIED BOUNDARY ELEMENT METHODS". PONTIFÍCIA UNIVERSIDADE CATÓLICA DO RIO DE JANEIRO, 2004. http://www.maxwell.vrac.puc-rio.br/Busca_etds.php?strSecao=resultado&nrSeq=5562@1.

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COORDENAÇÃO DE APERFEIÇOAMENTO DO PESSOAL DE ENSINO SUPERIOR
Apresentam-se as formulações, consolidando a nomenclatura e os principais conceitos dos métodos de elementos de contorno: convencional (MCCEC), híbrido de tensões (MHTEC), híbrido de deslocamentos (MHDEC) e híbrido simplificado de tensões (MHSTEC). proposto o método híbrido simplificado de deslocamentos (MHSDEC), em contrapartida ao MHSTEC, baseando-se nas mesmas hipóteses de aproximação de tensões e deslocamentos do MHDEC e supondo que a solução fundamental em termos de tensões seja válida no contorno. Como decorrência do MHSTEC e do MHSDEC, é apresentado também o método híbrido de malha reduzida dos elementos de contorno (MHMREC), com aplicação computacionalmente vantajosa a problemas no domínio da freqüência ou envolvendo materiais não-homogêneos. A partir da investigação das equações matriciais desses métodos, são identificadas quatro novas relações matriciais, das quais uma verifica-se como válida para a obtenção dos elementos das matrizes de flexibilidade e de deslocamento que não podem ser determinados por integração ou avaliação direta. Também é proposta a correta consideração, ainda não muito bem explicada na literatura, de que forças de superfície devem ser interpoladas em função de atributos de superfície e não de atributos nodais. São apresentadas aplicações numéricas para problemas de potencial para cada método mencionado, em que é verificada a validade das novas relações matriciais.
A consolidated, unified formulation of the conventional (CCBEM), hybrid stress (HSBEM), hybrid displacement (HDBEM) and simplified hybrid stress (SHSBEM) boundary element methods is presented. As a counterpart of SHSBEM, the simplified hybrid displacement boundary element method (SHDBEM) is proposed on the basis of the same stress and displacement approximation hypotheses of the HDBEM and on the assumption that stress fundamental solutions are also valid on the boundary. A combination of the SHSBEM and the SHDBEM gives rise to a provisorily called mesh-reduced hybrid boundary element method (MRHBEM), which seems computationally advantageous when applied to frequency domain problems or non-homogeneous materials. Four new matrix relations are identified, one of which may be used to obtain the flexibility and displacement matrix coefficients that cannot be determined by integration or direct evaluation. It is also proposed the correct consideration, still not well explained in the technical literature, that traction forces should be interpolated as functions of surface and not of nodal attributes. Numerical examples of potential problems are presented for each method, in which the validity of the new matrix relations is verified.

3

Uddin, Mudassir. "Interpretation of results from simplified principal components". Thesis, University of Aberdeen, 1999. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.301216.

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Linear multivariate statistical methods are widely used for analysing data sets which consist of a large number of variables. These techniques, which include principal component analysis, factor analysis, canonical correlation analysis, redundancy analysis and discriminant analysis, all produce a set of new variables, commonly called 'factors', according to some criterion which differs for different techniques. Among these techniques, principal component analysis is one of the most popular techniques used for reducing the dimensions of the multivariate data set. In many applications, when Principal Component Analysis (PCA) is performed on a large number of variables, the interpretation of the results is not simple. The derived eigenvectors of the sample covariance or correlation matrix are not necessarily in a simple form, with all coefficients either 'large' or 'negligible'. To aid interpretation, it is fairly common practice to rotate the retained set of components, often using orthogonal rotation. The purpose of rotation is to simplify structure, and thus to make it easier to interpret the low-dimensional space represented by the retained set of components. Thus, quantification of simplicity is a two step process. The first set involves the extraction of the feature from the data called components, while the second stage uses a rotation method to simplify the structure. One of the two main purposes of this thesis is to combine into one step these two separate stages of dimension reduction (finding the components) and simplification (rotation). This goal is achieved by combining these two objectives in the form of a single function leading to what we call Simplified Components (SCs). Another objective is to discover which of the many possible criteria suggested in factor analysis can be adopted in the proposed procedure of SCs. Thus, a simplified one-step procedure of SCs is proposed, using four measures of simplicity, namely varimax, quartimax, orthomax and equamax indices.

4

Veness, Raymond John Mark. "Simplified methods for the solution of thermal ratchetting problems". Thesis, University of Leicester, 1992. http://hdl.handle.net/2381/34716.

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This thesis presents a simple and conservative method for the analysis of inelastic cyclic thermal stress problems. It is developed for the analysis of severe cyclic thermal shocks combined with mechanical loads in thin walled tubes. The methods are intended to predict both the onset of ratchetting and the strains accumulated by small excursions into the ratchetting regime. The text begins by summarising the development of the upper bound shakedown theory-the main tool in this approach. Previous methods for simplified analysis using the upper bound method are reviewed and some ideas adopted. Building on this previous work, a new method of predicting the shakedown bound is developed. This is based on the upper bound analysis of particular ratchet mechanisms, resulting in a limiting equation for each mechanism. These equations are used to produce ratchet bounds for several thermal stress examples. These results are compared with the bounds produced by design code rules currently used for cyclic thermal stress. One observation reached in the prediction of these bounds was the lack of supporting evidence available. Therefore, a set of experiments were performed to show the bounds corresponding to two of these mechanisms. These used a new resistance heating method for applying the thermal cycles. The results are conservatively predicted by upper bound analysis. However, in some regions the effects of cyclic hardening reduces the strain accumulated, making the predictions over conservative. To investigate this effect some simple hardening rules are applied to the shakedown bounds. These are developed to give a prediction of accumulated strains within the ratchet region. Comparison is made both with the experiments and a finite element computer model. Finally, these predictions of shakedown and cyclic hardening controlled strain are combined to give a complete picture of cyclically heated tubes below the creep range.

5

Zhou, Ying Fu. "A study for orbit representation and simplified orbit determination methods". Thesis, Queensland University of Technology, 2003. https://eprints.qut.edu.au/15895/1/Ying_Fu_Zhou_Thesis.pdf.

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This research effort is concerned with the methods of simplified orbit determination and orbit representation and their applications for Low Earth Orbit (LEO) satellite missions, particularly addressing the operational needs of the FedSat mission. FedSat is the first Australian-built satellite in over thirty years. The microsatellite is approximately 50cm cubed with a mass of 58 kg. The satellite was successfully placed into a low-earth near-polar orbit at an altitude of 780km by the Japanese National Space Development Agency (NASDA) H-IIA launch vehicle on 14, December 2002. Since then, it has been streaming scientific data to its ground station in Adelaide almost daily. This information is used by Australian and international researchers to study space weather, to help improve the design of space computers, communication systems and other satellite technology, and for research into navigation and satellite tracking. This research effort addresses four practical issues regarding the FedSat mission and operations. First, unlike most satellite missions, the GPS receiver onboard FedSat operates in a duty-cycle mode due to the limitations of the FedSat power supply. This causes significant difficulties for orbit tracking, Precise Orbit Determination and scientific applications. A covariance analysis was performed before the mission launch to assess the orbit performance under different operational modes. The thesis presents the analysis methods and results. Second, FedSat supports Ka-band tracking experiments that require a pointing accuracy of 0.03 degree. The QUT GPS group is obligated to provide the GPS precise orbit solution to meet this requirement. Ka-band tracking requests satellite orbital position at any instant time with respect to any of the observation stations. Because orbit determination and prediction software only provide satellite orbital data at a discrete time point, it is necessary to find a way to represent the satellite orbit as a continuous trajectory with discrete observation data, able to obtain the position of the satellite at the time of interest. For this purpose, an orbit interpolation algorithm using the Chebyshev polynomial was developed and applied to Ka-band tracking applications. The thesis will describe the software and results. Third, since the launch of FedSat, investigators have received much flight GPS data. Some research was invested in the analysis of FedSat orbit performance, GPS data quality and the quality of the onboard navigation solutions. Studies have revealed that there are many gross errors in the FedSat onboard navigation solution (ONS). Although the 1-sigma accuracy of each component is about 20 m, there are more than 11 %positioning errors that fall outside +/-50m, and 5% of the errors are outside the 100mbound. The 3D RMS values would be 35m, 87m, and 173m for the above three cases respectively. The FedSat ONS uncertainties are believed to be approximately three times greater than those from other satellite missions. Due to the high percentage of outlier solutions, it would be dangerous to use these without first applying data detection and exclusion procedures. Therefore, this thesis presents two simplified orbit determination methods that can improve the ONS. One is the "geometric method", which makes use of delta-position solutions derived from carrier phase differences between two epochs to smooth the code-based navigation solutions. The algorithms were tested using SAC-C GPS data and showing some improvement. The second method is the "dynamic method", which uses orbit dynamics information for orbit improvements. Fourth, the FedSat ground tracking team at Adelaide use the NORAD TLE orbit for daily FedSat tracking. Research was undertaken to convert an orbit trajectory into these Two Line Elements (TLE). Algorithms for the estimation of TLE solutions from the FedSat onboard GPS navigation solutions are outlined. Numerical results have shown the effects of the unmodelled forces/perturbations in the SPG4 models for the FedSat orbit determination would reach a level of ±1000m. This only includes the orbit representation errors with TLE data sets. The total FedSat orbit propagation should include both the orbit propagation and orbit representation terms. The analysis also demonstrates that the orbit presentation error can be reduced to ±200m and ±100mlevels with the EGM4x4 and EGM10x10 gravity field models respectively. This can meet the requirements for Ka-band tracking. However, a simplified tracking program based on numerical integration has to be developed to replace the SPG4 models.

6

Zhou, Ying Fu. "A Study For Orbit Representation And Simplified Orbit Determination Methods". Queensland University of Technology, 2003. http://eprints.qut.edu.au/15895/.

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This research effort is concerned with the methods of simplified orbit determination and orbit representation and their applications for Low Earth Orbit (LEO) satellite missions, particularly addressing the operational needs of the FedSat mission. FedSat is the first Australian-built satellite in over thirty years. The microsatellite is approximately 50cm cubed with a mass of 58 kg. The satellite was successfully placed into a low-earth near-polar orbit at an altitude of 780km by the Japanese National Space Development Agency (NASDA) H-IIA launch vehicle on 14, December 2002. Since then, it has been streaming scientific data to its ground station in Adelaide almost daily. This information is used by Australian and international researchers to study space weather, to help improve the design of space computers, communication systems and other satellite technology, and for research into navigation and satellite tracking. This research effort addresses four practical issues regarding the FedSat mission and operations. First, unlike most satellite missions, the GPS receiver onboard FedSat operates in a duty-cycle mode due to the limitations of the FedSat power supply. This causes significant difficulties for orbit tracking, Precise Orbit Determination and scientific applications. A covariance analysis was performed before the mission launch to assess the orbit performance under different operational modes. The thesis presents the analysis methods and results. Second, FedSat supports Ka-band tracking experiments that require a pointing accuracy of 0.03 degree. The QUT GPS group is obligated to provide the GPS precise orbit solution to meet this requirement. Ka-band tracking requests satellite orbital position at any instant time with respect to any of the observation stations. Because orbit determination and prediction software only provide satellite orbital data at a discrete time point, it is necessary to find a way to represent the satellite orbit as a continuous trajectory with discrete observation data, able to obtain the position of the satellite at the time of interest. For this purpose, an orbit interpolation algorithm using the Chebyshev polynomial was developed and applied to Ka-band tracking applications. The thesis will describe the software and results. Third, since the launch of FedSat, investigators have received much flight GPS data. Some research was invested in the analysis of FedSat orbit performance, GPS data quality and the quality of the onboard navigation solutions. Studies have revealed that there are many gross errors in the FedSat onboard navigation solution (ONS). Although the 1-sigma accuracy of each component is about 20 m, there are more than 11 %positioning errors that fall outside +/-50m, and 5% of the errors are outside the 100mbound. The 3D RMS values would be 35m, 87m, and 173m for the above three cases respectively. The FedSat ONS uncertainties are believed to be approximately three times greater than those from other satellite missions. Due to the high percentage of outlier solutions, it would be dangerous to use these without first applying data detection and exclusion procedures. Therefore, this thesis presents two simplified orbit determination methods that can improve the ONS. One is the "geometric method", which makes use of delta-position solutions derived from carrier phase differences between two epochs to smooth the code-based navigation solutions. The algorithms were tested using SAC-C GPS data and showing some improvement. The second method is the "dynamic method", which uses orbit dynamics information for orbit improvements. Fourth, the FedSat ground tracking team at Adelaide use the NORAD TLE orbit for daily FedSat tracking. Research was undertaken to convert an orbit trajectory into these Two Line Elements (TLE). Algorithms for the estimation of TLE solutions from the FedSat onboard GPS navigation solutions are outlined. Numerical results have shown the effects of the unmodelled forces/perturbations in the SPG4 models for the FedSat orbit determination would reach a level of ±1000m. This only includes the orbit representation errors with TLE data sets. The total FedSat orbit propagation should include both the orbit propagation and orbit representation terms. The analysis also demonstrates that the orbit presentation error can be reduced to ±200m and ±100mlevels with the EGM4x4 and EGM10x10 gravity field models respectively. This can meet the requirements for Ka-band tracking. However, a simplified tracking program based on numerical integration has to be developed to replace the SPG4 models.

7

Wang, Yanchun. "Simplified methods for determining dynamic characteristics of tall wall-frame buildings". Thesis, University of Hertfordshire, 2000. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.323652.

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8

Valade, Rachel Elizabeth. "Development and verification of a simplified building energy model". Thesis, Atlanta, Ga. : Georgia Institute of Technology, 2009. http://hdl.handle.net/1853/28183.

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9

Alhaj, Hasan Ola. "Optimization of building energy consumption using simplified models and new control methods". Thesis, Lille 1, 2014. http://www.theses.fr/2014LIL10162/document.

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L'inquiétude croissante concernant le futur des ressources énergétique a fait de l'optimisation énergétique une priorité dans tous les secteurs. De nombreux sujets de recherche se sont focalisés sur celui du bâtiment étant le principal consommateur d'énergie, en particulier à cause de ses besoins en chauffage. Beaucoup de propositions pour réduire la consommations ont été faites. Ceux-ci vont de l'amélioration de l'isolation au changement du système de gestion du thermostat en passant par la formation des occupants à une meilleure gestion de leur bâtiment. Cette thèse propose une nouvelle méthode de contrôle qui permet de minimiser la consommation énergétique et dépenses budgétaires. La méthode génère un planning énergétique sur une période de temps pré-définie, ceci en prenant compte du confort thermique des occupants. Elle est basée sur l'application de la méthode de Monte Carlo, un générateur aléatoire appliqué au système de chauffage. L'objectif est de déterminer le planning de chauffage optimal, qui respecte les trois contraintes suivantes: - Le confort thermique des résidents; - La minimisation de l'énergie consommée / du budget; - Le déplacement de la charge. De plus, pour tester cette méthode, l'identification du comportement thermique du bâtiment a été requise. De ce fait, un modèle thermique du bâtiment a été développé. Ce modèle a été volontairement simplifié afin de l'intégrer plus simplement dans le processus de contrôle. De plus, une nouvelle approche d'identification thermique du bâtiment aussi bien qu'une nouvelle méthode de contrôle en temps réel ont été présentées
With the highly developing concerns about the future of energy resources, the optimization of energy consumption becomes a must in all sectors. A lot of research was dedicated to buildings regarding that they constitute the highest energy consuming sector mainly because of their heating needs. Many proposals of new strategies to minimize building consumption were done. These proposals vary between recommending better insulation, advising change in occupants' behavior and changing the heating control management. This thesis proposes a new control method that helps minimizing the heating consumption and expenses. This method generates an energy plan over a defined prediction horizon respecting the occupants’ thermal comfort. It is based on the application of Monte Carlo method, i.e., a random generator for the heating system scenarios. The aim is to determine the optimal heating plan for the prediction horizon that fulfills the constraints regarding the following three factors: • The thermal comfort of occupants; • The minimization of the energy consumption/expenses; • Load shifting. However, to test this method, an identification of the building thermal behavior was needed. Thus, a building thermal model to simulate the building behavior was developed. This model was meant to be simplified in order to better integrate it in the control process. Furthermore, a new parameter estimation approach as well as a real time temperature control method are presented to ensure the implementation of the optimal predicted plan

10

Larson, Mårten. "Estimation of crack risk in early age concrete : simplified methods for practical use". Licentiate thesis, Luleå tekniska universitet, 2000. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-25757.

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For many situations it is obvious that an understanding of how different types of cracks arise and methods to estimate the risk of early age cracking is needed. This thesis deals with parts of this phenomenon namely thermal through cracking caused by restraint from an adjoining structure. Different existing material models used in a thermal stress analysis are compared with a tested behaviour. The main work focus on evaluating simplified manual methods for thermal crack estimation that are based on direct formulations by means of the results from a more advanced differential type method. One of the studied methods is selected and formulated for practical use. Possilble measures against thermal cracking are described together with recommendations on how they may be implemented in the method. Comparisons with observations from full-scale castings give an indication about the accurary of the simplified method.
Godkänd; 2000; 20070318 (ysko)

Mais fontes

Livros sobre o assunto "Simplified methods":

1

Garza, Diana. Phlebotomy simplified. 2^a ed. Upper Saddle River, NJ: Pearson Education, 2013.

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2

Franchis, Roberto De. Capsule endoscopy simplified. Thorofare, NJ: SLACK, 2010.

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3

Takabatake, Hideo. Simplified Analytical Methods of Elastic Plates. Singapore: Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-0086-8.

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4

Amsden, Robert T. SPC simplified: Practical steps to quality. White Plains, N.Y: Quality Resources, 1989.

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5

Amsden, Robert T. SPC simplified: Practical steps to quality. White Plains, N.Y: Quality Resources, 1989.

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6

Maher, Andrea K. Simplified diet manual. Chichester, West Sussex, UK: Wiley-Blackwell, 2012.

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7

Goldberger, Ary Louis. Goldberger's clinical electrocardiography: A simplified approach. 8^a ed. Philadelphia, PA: Elsevier/Saunders, 2013.

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8

Bourges, Bernard. European simplified methods for active solar system design. Dordrecht, The Netherlands: Kluwer Academic Publishers, 1991.

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9

Amsden, Davida M. SPC simplified workbook: Practical steps to quality. White Plains, N.Y: Quality Resources, 1990.

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10

Garza, Diana. Phlebotomy simplified. Upper Saddle River, NJ: Pearson/Prentice Hall, 2008.

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Capítulos de livros sobre o assunto "Simplified methods":

1

Li, Zi Cai. "Simplified Hybrid Methods". In Combined Methods for Elliptic Equations with Singularities, Interfaces and Infinities, 251–80. Boston, MA: Springer US, 1998. http://dx.doi.org/10.1007/978-1-4613-3338-8_8.

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2

Morales-Espejel, G. E. "Simplified EHL Solution Methods". In Encyclopedia of Tribology, 3090–99. Boston, MA: Springer US, 2013. http://dx.doi.org/10.1007/978-0-387-92897-5_629.

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3

Atkins, Frank B., e Douglas Van Nostrand. "Simplified Methods of Dosimetry". In Thyroid Cancer, 651–56. New York, NY: Springer New York, 2016. http://dx.doi.org/10.1007/978-1-4939-3314-3_59.

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4

Church, James, e Graham Casey. "Molecular Genetics Methods Simplified". In Molecular Genetics of Colorectal Neoplasia, 27–44. Boston, MA: Springer US, 2004. http://dx.doi.org/10.1007/978-1-4419-9310-6_3.

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5

Okello, Gabriel Otieno. "Descriptive Statistics Methods". In Simplified Business Statistics Using SPSS, 37–126. Boca Raton: Chapman and Hall/CRC, 2022. http://dx.doi.org/10.1201/9781003292654-5.

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6

Kogel, Eric. "Rigid E-unification simplified". In Theorem Proving with Analytic Tableaux and Related Methods, 17–30. Berlin, Heidelberg: Springer Berlin Heidelberg, 1995. http://dx.doi.org/10.1007/3-540-59338-1_25.

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7

Winter, Kirsten, Chenyi Zhang, Ian J. Hayes, Nathan Keynes, Cristina Cifuentes e Lian Li. "Path-Sensitive Data Flow Analysis Simplified". In Formal Methods and Software Engineering, 415–30. Berlin, Heidelberg: Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-41202-8_27.

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8

Pironneau, Olivier. "Simplified Fluid-Structure Interactions for Hemodynamics". In Computational Methods in Applied Sciences, 57–70. Cham: Springer International Publishing, 2014. http://dx.doi.org/10.1007/978-3-319-06136-8_3.

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9

Kumar, Ritesh, Kartikeya Tiwari e Prakash Saudagar. "Simplified CRISPR-Mediated DNA Editing in Multicellular Eukaryotes". In Methods in Molecular Biology, 241–60. New York, NY: Springer US, 2022. http://dx.doi.org/10.1007/978-1-0716-2716-7_11.

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10

Takabatake, Hideo. "Static and Dynamic Analyses of Rectangular Normal Plates". In Simplified Analytical Methods of Elastic Plates, 3–24. Singapore: Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-13-0086-8_1.

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Trabalhos de conferências sobre o assunto "Simplified methods":

1

Perraud, Jean, Daniel Arnal, Gregoire Casalis, Jean-Pierre Archambaud e Raffaele Donelli. "Automatic Transition Predictions using Simplified Methods". In 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2009. http://dx.doi.org/10.2514/6.2009-1144.

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2

Polese, Maria, Marco Di Ludovico, Marco Gaetani d'Aragona e Andrea Prota. "REPAIRABILITY DECISIONS BASED ON SIMPLIFIED ASSESSMENT PROCEDURES". In 7th International Conference on Computational Methods in Structural Dynamics and Earthquake Engineering Methods in Structural Dynamics and Earthquake Engineering. Athens: Institute of Structural Analysis and Antiseismic Research School of Civil Engineering National Technical University of Athens (NTUA) Greece, 2019. http://dx.doi.org/10.7712/120119.6971.19602.

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3

Fratczak, Michal, Pawel Nowak e Jacek Czeczot. "Simplified modeling of plate heat exchangers". In 2014 19th International Conference on Methods & Models in Automation & Robotics (MMAR). IEEE, 2014. http://dx.doi.org/10.1109/mmar.2014.6957418.

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4

Yuan, Yong, e Haitao Yu. "SEISMIC ANALYSIS OF LONG TUNNEL: SIMPLIFIED OR UNIFIED". In 5th International Conference on Computational Methods in Structural Dynamics and Earthquake Engineering Methods in Structural Dynamics and Earthquake Engineering. Athens: Institute of Structural Analysis and Antiseismic Research School of Civil Engineering National Technical University of Athens (NTUA) Greece, 2015. http://dx.doi.org/10.7712/120115.3377.3008.

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5

Schmitter, Maximilian, e Christoph Adam. "SIMPLIFIED NUMERICAL MODELING STRATEGIES OF DEEP VIBRATORY COMPACTION". In 6th International Conference on Computational Methods in Structural Dynamics and Earthquake Engineering Methods in Structural Dynamics and Earthquake Engineering. Athens: Institute of Structural Analysis and Antiseismic Research School of Civil Engineering National Technical University of Athens (NTUA) Greece, 2017. http://dx.doi.org/10.7712/120117.5747.17293.

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6

Ke Xu, Behnam Shahrrava e Jianwei Wan. "Two simplified methods for linear turbo equalization". In 2009 Asia-Pacific Conference on Computational Intelligence and Industrial Applications (PACIIA 2009). IEEE, 2009. http://dx.doi.org/10.1109/paciia.2009.5406438.

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7

Yahalom, Asher. "CFD Methods Derived from Simplified Variational Principles". In 45th AIAA Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-315.

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8

"A Hybrid Local Search for Simplified Protein Structure Prediction". In International Conference on Bioinformatics Models, Methods and Algorithms. SciTePress - Science and and Technology Publications, 2013. http://dx.doi.org/10.5220/0004239401580163.

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9

Wang, Jue, Ding Zhou e Weiqing Liu. "SIMPLIFIED MODEL FOR COUPLED VIBRATION OF ADJACENT STRIP FOOTINGS". In 5th International Conference on Computational Methods in Structural Dynamics and Earthquake Engineering Methods in Structural Dynamics and Earthquake Engineering. Athens: Institute of Structural Analysis and Antiseismic Research School of Civil Engineering National Technical University of Athens (NTUA) Greece, 2015. http://dx.doi.org/10.7712/120115.3694.742.

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10

Vimmr, Jan, Ondrej Bublik, Ales Pecka e Ludek Pesek. "NUMERICAL ANALYSIS OF FLUTTER INSTABILITY IN SIMPLIFIED BLADE CASCADE". In 6th International Conference on Computational Methods in Structural Dynamics and Earthquake Engineering Methods in Structural Dynamics and Earthquake Engineering. Athens: Institute of Structural Analysis and Antiseismic Research School of Civil Engineering National Technical University of Athens (NTUA) Greece, 2017. http://dx.doi.org/10.7712/120117.5685.17525.

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Relatórios de organizações sobre o assunto "Simplified methods":

1

Hurel, Nolwenn, Max H. Sherman e Iain S. Walker. Simplified Methods for Combining Natural and Mechanical Ventilation. Office of Scientific and Technical Information (OSTI), junho de 2015. http://dx.doi.org/10.2172/1469162.

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2

Hurel, Nolwenn, Max H. Sherman e Iain S. Walker. Simplified Methods for Combining Natural and Mechanical Ventilation. Office of Scientific and Technical Information (OSTI), junho de 2015. http://dx.doi.org/10.2172/1512199.

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3

Tai Asayama. Update and Improve Subsection NH ?? Alternative Simplified Creep-Fatigue Design Methods. Office of Scientific and Technical Information (OSTI), outubro de 2009. http://dx.doi.org/10.2172/974288.

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4

Jeries J. Abou-Hanna, Douglas L. Marriott e Timothy E. McGreevy. Update and Improve Subsection NH - Simplified Elastic and Inelastic Design Analysis Methods. Office of Scientific and Technical Information (OSTI), junho de 2009. http://dx.doi.org/10.2172/974287.

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5

Bhuiyan, S. I., R. W. Roussin, J. L. Lucius, J. H. Marable e D. A. Bartine. Development of simplified methods and data bases for radiation shielding calculations for concrete. Office of Scientific and Technical Information (OSTI), junho de 1986. http://dx.doi.org/10.2172/5629265.

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6

Messner, M. C., e T. L. Sham. Development of ASME Division 5 Code proposal on temperature limits for simplified design methods. Office of Scientific and Technical Information (OSTI), julho de 2018. http://dx.doi.org/10.2172/1480531.

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7

Choquette, Gary, e Nolan Choquette. PR-000-16600-R01 Correlative Estimation of Hydrocarbon Dewpoint. Chantilly, Virginia: Pipeline Research Council International, Inc. (PRCI), setembro de 2019. http://dx.doi.org/10.55274/r0011618.

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Resumo:

Simplified methods to estimate the hydrocarbon cricondentherm hydrocarbon dewpoint temperature and the associated phase curve are desirable in cases with limited processor power/memory or in cases where full gas composition analysis information is not available. This study developed and evaluated several methods to provide reasonable estimates of hydrocarbon dew-point temperature and the phase curve using simplified correlation methods.

8

Walker, Iain S., Craig P. Wray, Cyril Guillot e S. Masson. Evaluation of commercially available techniques and development of simplified methods for measuring grille airflows in HVAC systems. Office of Scientific and Technical Information (OSTI), agosto de 2003. http://dx.doi.org/10.2172/819472.

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9

Miller, Wayne, e William Welch. Demonstration of Simplified Field Test Methods for the Measurement of Diesel Particulate Matter (PM) from Military Diesel Engines. Fort Belvoir, VA: Defense Technical Information Center, julho de 2008. http://dx.doi.org/10.21236/ada531078.

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10

Tompson, A., M. Zavarin, C. Bruton e G. Pawloski. Methods for Calculating a Simplified Hydrologic Source Term for Frenchman Flat Sensitivity Studies of Radionuclide Transport Away from Underground Nuclear Tests. Office of Scientific and Technical Information (OSTI), janeiro de 2004. http://dx.doi.org/10.2172/15009761.

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