Relevant bibliographies by topics / Hot Holes Injection Erasing

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  1. Journal articles

Academic literature on the topic 'Hot Holes Injection Erasing'

Author: Grafiati
Published: 25 May 2024

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Journal articles on the topic "Hot Holes Injection Erasing"

1

Chen, Shen Li, and Shun Tai Chung. "Charge Programming and Erasing Characteristics of the Submicron Stacked-Gate Flash Cells." Advanced Materials Research 634-638 (January 2013): 2446–49. http://dx.doi.org/10.4028/www.scientific.net/amr.634-638.2446.

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A non-Maxwellian hot-carrier generation current model for simulation of charge injection and erasing in the 0.35um flash EEPROM device is presented in this paper. Unlike the conventional model, which is based on the local electric fields in the device, and it accounts for non-local effects resulting from the large variations in electric field in a submicron flash EEPROM. Good agreements between the measured and calculated results in the charge writing and the Fower-Nordheim erasing operations.
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2

Jin, Yuxuan, and Zefeng Chen. "High gain hot-carrier WSe2 phototransistor with gate-tunable responsivity." Advances in Engineering Technology Research 7, no. 1 (2023): 21. http://dx.doi.org/10.56028/aetr.7.1.21.2023.

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Hot-carrier injection at semiconductor/metal interface shows great potentials in infrared photodetection. However, the photoresponsivity of hot-carrier photodetector with diode mode is still limited in the scale of 1 mA/W due to the low injection efficiency of hot carriers and the lack of gain. Here, we demonstrate a high gain hot-carrier WSe2 phototransistor with gate-tunable responsivity. In this device, plasmonic resonances is used to enhance the light absorption of gold nanodisk, which provide hot holes. The hot holes are trapped into WSe2 and recycled in WSe2 channel in lateral direction,
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3

Sun, Lei, Liyang Pan, Huiqing Pang, et al. "Characteristics of Band-to-Band Tunneling Hot Hole Injection for Erasing Operation in Charge-Trapping Memory." Japanese Journal of Applied Physics 45, no. 4B (2006): 3179–84. http://dx.doi.org/10.1143/jjap.45.3179.

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4

Manzini, S., and A. Gallerano. "Avalanche injection of hot holes in the gate oxide of LDMOS transistors." Solid-State Electronics 44, no. 7 (2000): 1325–30. http://dx.doi.org/10.1016/s0038-1101(99)00317-2.

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5

Jeong, Yoon Seong, and Jun Su Park. "Effect of Inlet Compound Angle of Backward Injection Film Cooling Hole." Energies 13, no. 4 (2020): 808. http://dx.doi.org/10.3390/en13040808.

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Backward injection film cooling holes were studied to improve film cooling effectiveness using simple cylindrical holes, and this principle was applied to an actual gas turbine. Although film cooling effectiveness was improved using a backward injection film cooling hole, the backward flow of combustion gas from the backward injection cooling hole was one of the major reasons for cracks in the hot components. To prevent cracks and backward flow in the backward injection film cooling hole, this study changed the inlet compound angle of the backward injection film cooling hole. Numerical analysi
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6

Williamson, J. G., H. van Houten, C. W. J. Beenakker, et al. "Injection of ballistic hot electrons and cool holes in a two-dimensional electron gas." Surface Science 229, no. 1-3 (1990): 303–6. http://dx.doi.org/10.1016/0039-6028(90)90894-e.

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7

Liu, Jian, Mengyao Xu, and Wenxiong Xi. "Effects of Gas Thermophysical Properties on the Full-Range Endwall Film Cooling of a Turbine Vane." Aerospace 10, no. 7 (2023): 592. http://dx.doi.org/10.3390/aerospace10070592.

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To protect turbine endwall from heat damage of hot exhaust gas, film cooling is the most significant method. The complex vortex structures on the endwall, such as the development of horseshoe vortices and transverse flow, affects cooling coverage on the endwall. In this study, the effects of gas thermophysical properties on full-range endwall film cooling of a turbine vane are investigated. Three kinds of gas thermophysical properties models are considered, i.e., the constant property gas model, ideal gas model, and real gas model, with six full-range endwall film cooling holes patterns based
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8

Lin, Y. L., and T. I. P. Shih. "Film Cooling of a Cylindrical Leading Edge With Injection Through Rows of Compound-Angle Holes." Journal of Heat Transfer 123, no. 4 (2001): 645–54. http://dx.doi.org/10.1115/1.1370513.

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Computations, based on the k-ω shear-stress transport (SST) turbulence model in which all conservation equations were integrated to the wall, were performed to investigate the three-dimensional flow and heat transfer about a semi-cylindrical leading edge with a flat afterbody that is cooled by film-cooling jets, injected from a plenum through three staggered rows of compound-angle holes with one row along the stagnation line and two rows along ±25 deg. Results are presented for the surface adiabatic effectiveness, normalized temperature distribution, velocity vector field, and surface pressure
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9

Gustafsson, K. M. Bernhard, and T. Gunnar Johansson. "An Experimental Study of Surface Temperature Distribution on Effusion-Cooled Plates." Journal of Engineering for Gas Turbines and Power 123, no. 2 (2001): 308–16. http://dx.doi.org/10.1115/1.1364496.

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A parametric study of temperature distribution on effusion-cooled plates under conditions typical for combustion chambers was performed using infrared thermography. In this investigation, the effects of different temperature ratios, velocity ratios of the two air streams, the injection hole spacing, inclination angle of the injection holes, and the thermal heat conductivity of the plates were studied. For a given amount of cooling air, the cooling efficiency was found to increase markedly with a reduction in hole spacing, i.e., when the number of holes was increased. Reducing the injection ang
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10

Kafaei, Amir, Fahime Salmani, Esmail Lakzian, Włodzimierz Wróblewski, Mikhail S. Vlaskin, and Qinghua Deng. "The best angle of hot steam injection holes in the 3D steam turbine blade cascade." International Journal of Thermal Sciences 173 (March 2022): 107387. http://dx.doi.org/10.1016/j.ijthermalsci.2021.107387.

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