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Relevant bibliographies by topics / PARAMETRIC INVESTIGATION

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Academic literature on the topic 'PARAMETRIC INVESTIGATION'

Author: Grafiati

Published: 11 September 2023

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Journal articles on the topic "PARAMETRIC INVESTIGATION"

1

Poladian, Sajad, and Farshad Farahbod. "Parametric investigation of moving properties of zinc oxide nano-fluid." Scholars Academic Journal of Biosciences 4, no. 7 (2016): 555–59. http://dx.doi.org/10.21276/sajb.2016.4.7.1.

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2

Hegab, Hassan I. A. "Parametric Investigation of Cable‐Stayed Bridges." Journal of Structural Engineering 114, no. 8 (1988): 1917–28. http://dx.doi.org/10.1061/(asce)0733-9445(1988)114:8(1917).

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3

Iyer, Nandini, Babette Eaton, and Ramkumar Sridharan. "Parametric investigation of the virtual glide." Journal of the Acoustical Society of America 106, no. 4 (1999): 2209. http://dx.doi.org/10.1121/1.427504.

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4

Hung, Hazel S. S., Jerry Prawiharjo, Nikita K. Daga, David C. Hanna, and David P. Shepherd. "Experimental investigation of parametric transfer in synchronously pumped optical parametric oscillators." Journal of the Optical Society of America B 24, no. 12 (2007): 2998. http://dx.doi.org/10.1364/josab.24.002998.

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5

Liao, Yan Ping, Li Liu, and Teng Long. "Investigation of Various Parametric Geometry Representation Methods for Airfoils." Applied Mechanics and Materials 110-116 (October 2011): 3040–46. http://dx.doi.org/10.4028/www.scientific.net/amm.110-116.3040.

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Abstract—This paper presents the investigation of typical parametric geometry representation methods for airfoils, namely, PARSEC method, orthogonal basis function method and CST method. The investigation assesses the fitting accuracy of these parametric methods for various airfoils including the symmetric airfoil, cambered airfoil and supercritical airfoil. The design variables of these parametric methods are solved by the methods of least squares fit. The fitting results show that the fitting accuracy of CST method is better than other parametric methods for airfoil. The aerodynamics analysis models of these typical parametric geometry representation methods for airfoil are constructed. The pressure distributions calculated for different parametric methods are compared with the corresponding experimental pressure distributions for the actual airfoil geometry.Keywords-orthogonal basis function; PARSEC; CST; fitting accuracy; pressure distributions

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6

Babanov, N. Yu, A. V. Klyuev, S. V. Lartsov, and V. P. Samarin. "Investigation of stripline parametric passive radio transponders." IOP Conference Series: Materials Science and Engineering 1047, no. 1 (2021): 012073. http://dx.doi.org/10.1088/1757-899x/1047/1/012073.

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7

Yap, Hiew Thong, Su Kong Ngien, Norasman Bin Othman, Nadiatul Adilah Binti Ahmad Abdul Ghani, and Norhan Bin Abd Rahman. "Parametric investigation in Malaysian separate sewer systems." Proceedings of the Institution of Civil Engineers - Municipal Engineer 170, no. 2 (2017): 90–96. http://dx.doi.org/10.1680/jmuen.16.00019.

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Dafni, Jacob, and Joseph Wartman. "Centrifuge Studies of Topographic Effects: Parametric Investigation." Bulletin of the Seismological Society of America 111, no. 4 (2021): 2087–100. http://dx.doi.org/10.1785/0120200354.

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ABSTRACT This article presents the results of a comprehensive geotechnical centrifuge experimental program to investigate topographic effects across a series of single-sided slopes. The experimental campaign considered a range of governing factors, including slope inclination and ground-motion amplitude, frequency content, and duration. The testing program was nondestructive, allowing the centrifuge models to be subjected to over 140 different ground motions. Clear evidence of topographic effects, including amplification and deamplification of ground motion, were observed. Topography modified the frequency content and amplitude of the ground motion such that at the slope crest (1) peak ground accelerations ranged from 50% less than to 200% greater than the free-field, and (2) ground-motion mean square frequency shifted by as much as 55%. Higher topographic amplification levels lead to a larger topographic zone of influence, which, on average, spanned a distance equal to the slope height (H) behind and 2H in front of (toward slope) the slope crest. Physical modeling in the centrifuge proved to be a powerful experimental technique for generating empirical data to analyze topographic effects in a systematic and repeatable manner.

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Daqaq, Mohammed F., Christopher Stabler, Yousef Qaroush, and Thiago Seuaciuc-Osório. "Investigation of Power Harvesting via Parametric Excitations." Journal of Intelligent Material Systems and Structures 20, no. 5 (2008): 545–57. http://dx.doi.org/10.1177/1045389x08100978.

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This article presents an analytical and experimental investigation of energy harvesting via parametrically excited cantilever beams. To that end, we consider a lumped-parameter non-linear model that describes the first-mode dynamics of a parametrically excited cantilever-type harvester. The model accounts for the beam's geometric and inertia non-linearities as well as non-linearities representing air drag. Using the method of multiple scales, we obtain approximate analytical expressions describing the beam response, voltage drop across a purely resistive load, and output power in the vicinity of the first principle parametric resonance. Using these expressions, we study the effect of the electromechanical coupling and load resistance on the output power. We show that these parameters play an imperative role in determining the magnitude of the output power and characterizing the broad-band properties of the harvester. Specifically, we show that the region of parametric instability wherein energy can be harvested shrinks as the coupling coefficient increases. Furthermore, we show that there exists a coupling coefficient beyond which the peak power decreases. We also demonstrate that there is a critical excitation level below which no energy can be harvested. The amplitude of this critical excitation increases with the coupling coefficient and is maximized for a given load resistance. Theoretical findings that were compared to experimental results show good agreement and reflect the general trends.

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10

Conroy, P. J., P. Weinacht, and M. J. Nusca. "Parametric Erosion Investigation: Propellant Adiabatic Flame Temperature." Defence Science Journal 52, no. 1 (2002): 77–85. http://dx.doi.org/10.14429/dsj.52.2152.

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