Relevant bibliographies by topics / PLASMA SHEATH

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  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'PLASMA SHEATH'

Author: Grafiati
Published: 4 June 2021
Last updated: 25 January 2023

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Journal articles on the topic "PLASMA SHEATH"

1

Shaikh, Zubair I., Anil N. Raghav, Geeta Vichare, Ankush Bhaskar, and Wageesh Mishra. "Comparative statistical study of characteristics of plasma in planar and non-planar ICME sheaths during solar cycles 23 and 24." Monthly Notices of the Royal Astronomical Society 494, no. 2 (April 22, 2020): 2498–508. http://dx.doi.org/10.1093/mnras/staa783.

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ABSTRACT Planar magnetic structures (PMS) are often observed in sheath regions driven by interplanetary coronal mass ejections (ICMEs) and in corotating interaction regions (CIRs). Here, we study plasma properties statistically within planar and non-planar ICME sheath regions using in situ data from the Advanced Composition Explore (ACE) spacecraft. The study includes 420 ICME-driven sheaths from 1998–2017. We found that 146 ($\sim 35{{\ \rm per\ cent}}$) ICME-driven sheaths are planar, whereas 274 ($\sim 65{{\ \rm per\ cent}}$) are non-planar. This study found that the average plasma temperature, density, speed, plasma beta, thermal pressure and magnetic pressure are higher in planar sheaths than in non-planar sheaths. This implies that high compression plays an essential role in the formation of PMS in sheath regions. Interestingly, our analysis reveals explicitly that the strength of the southward/northward magnetic field component is almost double in planar sheath regions compared with non-planar sheath regions. This suggests that planar sheaths are more geoeffective than non-planar sheaths.
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Das, G. C., R. Deka, and M. P. Bora. "Revisiting the plasma sheath—dust in plasma sheath." Physics of Plasmas 23, no. 4 (April 2016): 042308. http://dx.doi.org/10.1063/1.4946865.

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Ala-Lahti, Matti M., Emilia K. J. Kilpua, Andrew P. Dimmock, Adnane Osmane, Tuija Pulkkinen, and Jan Souček. "Statistical analysis of mirror mode waves in sheath regions driven by interplanetary coronal mass ejection." Annales Geophysicae 36, no. 3 (May 24, 2018): 793–808. http://dx.doi.org/10.5194/angeo-36-793-2018.

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Abstract. We present a comprehensive statistical analysis of mirror mode waves and the properties of their plasma surroundings in sheath regions driven by interplanetary coronal mass ejection (ICME). We have constructed a semi-automated method to identify mirror modes from the magnetic field data. We analyze 91 ICME sheath regions from January 1997 to April 2015 using data from the Wind spacecraft. The results imply that similarly to planetary magnetosheaths, mirror modes are also common structures in ICME sheaths. However, they occur almost exclusively as dip-like structures and in mirror stable plasma. We observe mirror modes throughout the sheath, from the bow shock to the ICME leading edge, but their amplitudes are largest closest to the shock. We also find that the shock strength (measured by Alfvén Mach number) is the most important parameter in controlling the occurrence of mirror modes. Our findings suggest that in ICME sheaths the dominant source of free energy for mirror mode generation is the shock compression. We also suggest that mirror modes that are found deeper in the sheath are remnants from earlier times of the sheath evolution, generated also in the vicinity of the shock. Keywords. Interplanetary physics (plasma waves and turbulence; solar wind plasma) – space plasma physics (waves and instabilities)
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Main, Geoffrey L., and S. H. Lam. "A general solution condition for collisionless sheaths." Journal of Plasma Physics 38, no. 2 (October 1987): 287–300. http://dx.doi.org/10.1017/s0022377800012587.

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A general solution condition for collisionless sheaths is developed. Previous work has assumed that the Bohm criterion or the generalized Bohm criterion ensures a self-consistent sheath solution. This paper shows that for nonmonotonic collisionless sheath structures, such as double sheaths containing trapped ions, the generalized Bohm criterion is a necessary but not a sufficient condition. The general solution condition developed is always sufficient and the generalized Bohm criterion is shown to be special case of it. The general solution condition is applied to a double emitter sheath containing trapped ions. First, it is shown that the low-energy part of the plasma ion distribution coming into the sheath cannot be neglected as claimed in some analyses, because the shift in mean ion velocity through the pre-sheath (generalized Bohm speed) depends strongly on low-energy ions. Second, it is shown that the presence of trapped ions moves the point of critical self-consistency away from the collisionless sheath-neutral plasma asymptotic match and into the collisionless sheath. Consequently, both the sheath structure and the generalized Bohm speed depend on the amount of trapped ions. Thus collisional effects may dominate the structure of a presumably collisionless sheath through the trapping mechanism and the collisional pre-sheath which determines the low-energy ion component entering the collisionless sheath.
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Riemann, K.-U. "Plasma and sheath." Plasma Sources Science and Technology 18, no. 1 (November 14, 2008): 014006. http://dx.doi.org/10.1088/0963-0252/18/1/014006.

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Xing, Yunqi, Yixuan Wang, Jiakai Chi, Haoliang Liu, and Jin Li. "Study on Improving Interface Performance of HVDC Composite Insulators by Plasma Etching." Coatings 10, no. 11 (October 27, 2020): 1036. http://dx.doi.org/10.3390/coatings10111036.

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High-voltage direct-current composite insulators are faced with various challenges during operation, such as creeping discharge, umbrella skirt damage, abnormal heating and insulator breakage. Among them, the aging of the interface between the core rod and the sheath is one of the important causes of composite insulator failure. In order to improve the electrical resistance of the composite insulator interface, this study uses plasma etching to modify the surface of the glass-fiber-reinforced epoxy resin plastic to prepare the high-voltage direct-current composite insulator core rod–sheath samples. By analyzing the surface morphology of the epoxy resin, static contact angle and surface charge transfer characteristics, the control mechanism of the plasma etching treatment on the interface bonding performance and leakage current of composite insulator core rod–sheath samples were studied. The results show that proper etching time treatment can improve the trap energy level distribution and microstructure of epoxy resin and increase the discharge voltage along the surface; chemical bonding plasma etching can improve the interfacial bonding performance of core rod–sheath samples sheaths, reduce the leakage current of composite insulator core rod–sheath samples sheath specimens and improve their interfacial performance.
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Lavine, E. S., S. V. R. Rocco, W. M. Potter, J. Angel, E. Freeman, J. T. Banasek, J. Lawson, et al. "Measurements of the imploding plasma sheath in triple-nozzle gas-puff z pinches." Physics of Plasmas 29, no. 6 (June 2022): 062702. http://dx.doi.org/10.1063/5.0084352.

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Gas-puff z-pinch implosions are characterized by the formation of a dense annular plasma shell, the sheath, that is driven to the axis by magnetic forces and therefore subject to the magneto-Rayleigh–Taylor instability. Here, the conditions within these sheaths are measured on the 1-MA COBRA generator at Cornell University [Greenly et al., Rev. Sci. Instrum. 79, 073501 (2008)] for various gas species and initial fill densities. The gas-puff loads are initialized by a 7 cm diameter triple-nozzle gas valve assembly with concentric outer and inner annular nozzles and a central gas jet. Thomson scattering and laser interferometry provide spatially resolved flow, temperature, and electron density profiles midway through the implosion, while extreme ultraviolet pinhole cameras record the evolution of the plasma column and photoconducting diodes measure x-ray emission. Analysis of the scattering spectra includes a means of discriminating between thermal and non-thermal broadening to test for the presence of hydrodynamic turbulence. Two types of sheath profiles are observed, those with sharp discontinuities at the leading edge and those with smooth gradients. In both cases, non-thermal broadening is generally peaked at the front of the sheath and exhibits a characteristic decay length that roughly scales with the sheath ion mean free path. We demonstrate that this non-thermal broadening term is inconsistent with laminar velocity gradients and is more consistent with dissipative turbulence driven by unstable plasma waves in a collisionless shock. The resulting differences in sheath profile are then set by the sheath ion collisionality in a manner consistent with recent 1D kinetic simulations [Angus et al., Phys. Plasmas 28, 010701 (2021)].
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Stenzel, Reiner L., Johannes Grünwald, Codrina Ionita, Roman Schrittwieser, and Manuel Urrutia. "Sheaths and Double Layers with Instabilities." Journal of Technological and Space Plasmas 2, no. 1 (March 24, 2021): 70–92. http://dx.doi.org/10.31281/jtsp.v2i1.16.

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The properties of sheaths and associated potential structures and instabilities cover a broad field which even a review cannot cover everything. Thus, the focus will be on about a dozen examples, describe their observations and focus on the basic physical explanations for the effects, while further details are found in the references. Due to familiarity the review focuses mainly on the authors work but compared and referenced related work. The topics start with a high frequency oscillations near the electron plasma frequency. Low frequency instabilities also occur at the ion plasma frequency.The injection of ions into an electron-rich sheath widens the sheath and forms a double layer. Likewise, the injection of electrons into an ion rich sheath widens and establishes a double layer which occurs in free plasma injection into vacuum. The sheath widens and forms a double layer by ionization in an electron rich sheath. When particle fluxes in "fireballs" gets out of balance the double layer performs relaxation instabilities which has been studied extensively. Fireballs inside spherical electrodes create a new instability due to the transit time of trapped electrons. On cylindrical and spherical electrodes the electron rich sheath rotates in magnetized plasmas. Electrons rotate due to $\mathbf E \times \mathbf B_0$ which excites electron drift waves with azimuthal eigenmodes. Conversely a permanent magnetic dipole has been used as a negative electrode. The impact of energetic ions produces secondary electron emission, forming a ring of plasma around the magnetic equator. Such "magnetrons" are subject to various instabilities. Finally, the current to a positively biased electrode in a uniformly magnetized plasma is unstable to relaxation oscillations, which shows an example of global effects. The sheath at the electrode raises the potential in the flux tube of the electrode thereby creating a radial sheath which moves unmagnetized ions radially. The ion motion creates a density perturbation which affects the electrode current. If the electrode draws large currents the current disruptions create large inductive voltages on the electrode, which again produce double layers. This phenomenon has been seen in reconnection currents. Many examples of sheath properties will be explained. Although the focus is on the physics some examples of applications will be suggested such as neutral gas heating and accelerating, sputtering of plasma magnetrons and rf oscillators.
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Ghomi, Hamid, Mansour Khoramabadi, Padma Kant Shukla, and Mahmod Ghorannevis. "Plasma sheath criterion in thermal electronegative plasmas." Journal of Applied Physics 108, no. 6 (September 15, 2010): 063302. http://dx.doi.org/10.1063/1.3475508.

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Yang, Xiaocui, Kai Yuan, Yuhao Wang, and Mingyang Mao. "Numerical modeling on the bit error rate of EHF communication in time-varying hypersonic plasma sheath." AIP Advances 12, no. 4 (April 1, 2022): 045318. http://dx.doi.org/10.1063/5.0087974.

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Plasma sheaths enveloping hypersonic vehicles could yield a communication blackout. Many previous studies have shown that the electromagnetic wave in an extremely high frequency (EHF) band could penetrate a hypersonic plasma sheath effectively. In other words, the EHF communication could be a potential solution to the communication blackout problem. Nevertheless, most of those works used to concern only the EHF signal attenuation. In addition, those works normally treated plasma sheaths as a static plasma layer. However, plasma sheaths always keep evolving. In the present study, the modulated EHF signal propagation in a time-varying plasma sheath was investigated numerically. The plasma sheath was obtained with a hypersonic hydrodynamical model that has been utilized in previous studies. The EHF signal propagation was modeled based on theories of geometrical optics. The frequencies studied are 94, 140, and 225 GHz. The investigation revealed that not only signal attenuation but also the phase shifts for carrier waves vary with time. Their impact on the bit error rate (BER) of the EHF communication system was studied numerically. The modulation modes concerned in the present study are 2ASK, 2PSK, 4QAM, and Non-Coherent demodulation 2FSK (NC-2FSK). According to the study, the BER keeps varying with time. This study also showed that the BER is impacted by the carrier frequency, modulation mode, and the demodulation method. According to the comparison and the analysis, the suggested modulation modes are 2PSK and 4QAM at the carrier frequency of 140 GHz, which could lead to smaller and more stable BER for the EHF communication system utilized by hypersonic vehicles.
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Dissertations / Theses on the topic "PLASMA SHEATH"

1

Riggs, John Forrest. "Anode sheath contributions in plasma thrusters." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1994. http://handle.dtic.mil/100.2/ADA280395.

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Thesis (Degrees of Aeronautical & Astronautical Engineer and M.S. in Astronautical Engineering) Naval Postgraduate School, March 1994.
Thesis advisor(s): Oscar Biblarz. "March 1994." Includes bibliographical references. Also available online.
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Kawamura, Gakushi. "Gyrokinetic Theory for Peripheral Plasmas and its Application to Plasma Sheath." 京都大学 (Kyoto University), 2008. http://hdl.handle.net/2433/57265.

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Starkey, Ryan P., Mark J. Lewis, and Charles H. Jones. "PLASMA SHEATH CHARACTERIZATION FOR TELEMETRY IN HYPERSONIC FLIGHT." International Foundation for Telemetering, 2003. http://hdl.handle.net/10150/606733.

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International Telemetering Conference Proceedings / October 20-23, 2003 / Riviera Hotel and Convention Center, Las Vegas, Nevada
During certain hypersonic flight regimes, shock heating of air creates a plasma sheath resulting in telemetry attenuation or blackout. The severity of the signal attenuation is dependent on vehicle configuration, flight trajectory, and transmission frequency. This phenomenon is investigated with a focus placed on the nonequilibrium plasma sheath properties (electron concentration, plasma frequency, collision frequency, and temperature) for a range of flight conditions and vehicle design considerations. Trajectory and transmission frequency requirements for air-breathing hypersonic vehicle design are then addressed, with comparisons made to both shuttle orbiter and RAM-C II reentry flights.
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Figueroa, Shana Suzanne. "Ion scattering in a self-consistent cylindrical plasma sheath." Link to electronic thesis, 2006. http://www.wpi.edu/Pubs/ETD/Available/etd-051006-112304/.

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Thesis (M.S.)--Worcester Polytechnic Institute.
Keywords: orbital trajectory, ion collection, turning point method, spherical probes, turning angle, ion scattering, cylindrical probes. Includes bibliographical references (p.60-63).
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Brown, George Scott. "Exploring plasma sheath solutions for planar and cylindrical anodes." Thesis, Monterey, California. Naval Postgraduate School, 1991. http://hdl.handle.net/10945/43771.

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Anode sheaths impact the operation of many practical plasma devices. This complex region is explored in detail for collisional, isothermal (identical specie temperatures), low-temperature plasmas, where sheath dimensions are in the micron range. The selected approach involves postulation of a specific electric field distribution with two shape factors. Previous research regarding planar anodes is verified and expanded upon using greater parameter ranges. 'Z', a dimensionless quantity specifying plasma composition and condition, groups diverse plasmas into 'families' exhibiting similar sheath characteristics. Eta, a nondimensional ratio of electrical energy to thermal energy in the sheath, allows temperature effects to be studied. The investigation focuses on three disparate plasma families that span a range of 1.1729 to 2,1493, at eta values defined by plasma temperatures of 6000 K, 3000 K, and 3000 K. Results indicate that at lower temperatures, charge production in the outer sheath is generic to the electric field distribution, and that the sheaths themselves are nearly unaffected by substantial changes in temperature (i.e., eta). Conversely, sheath density and extent are shown to vary significantly for differing z values. Newly-derived equations governing cylindrical anodes generate sheaths that are virtually identical to corresponding planar cases. It is shown that only those anodes whose radii are comparable to the plasma's characteristic radius (gamma) must be treated with the cylindrical formulation; non-vacuous plasma would require micron-width anodes to be thus affected. Finally, an analytical approach yields solutions that confirm the numerical results, and offers an algebraic approximation for high-eta plasmas.
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Han, W. E. "The stability of the plasma sheath with secondary emission." Thesis, City University London, 1988. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.382894.

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Takamura, S., T. Misawa, N. Ohno, S. Nunomura, M. Sawai, K. Asano, and P. K. Kaw. "Dynamic behaviors of dust particles in the plasma–sheath boundary." American Institute of Physics, 2001. http://hdl.handle.net/2237/7044.

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Taneda, Hiroshi. "The effect of a plasma sheath on hypersonic flight communications." Thesis, Massachusetts Institute of Technology, 1990. http://hdl.handle.net/1721.1/42438.

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Ku, Victor Po-Tsung. "Experimental studies of capacitively coupled RF discharges." Thesis, University of Oxford, 1996. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.318752.

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Langendorf, Samuel J. "Effects of electron emission on plasma sheaths." Diss., Georgia Institute of Technology, 2015. http://hdl.handle.net/1853/54383.

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Current state-of-the-art plasma thrusters are limited in power density and thrust density by power losses to plasma-facing walls and electrodes. In the case of Hall effect thrusters, power deposition to the discharge channel walls and anode negatively impact the efficiency of the thruster and limit the attainable power density and thrust density. The current work aims to recreate thruster-relevant wall-interaction physics in a quiescent plasma and investigate them using electrostatic probes, in order to inform the development of the next generation of high-power-density / high-thrust-density propulsion devices. Thruster plasma-wall interactions are complicated by the occurrence of the plasma sheath, a thin boundary layer that forms between a plasma and its bounding wall where electrostatic forces dominate. Sheaths have been recognized since the seminal work of Langmuir in the early 1900’s, and the theory of sheaths has been greatly developed to the present day. The theories are scalable across a wide range of plasma parameters, but due to the difficulty of obtaining experimental measurements of plasma properties in the sheath region, there is little experimental data available to directly support the theoretical development. Sheaths are difficult to measure in situ in thrusters due to the small physical length scale of the sheath (order of micrometers in thruster plasmas) and the harsh plasma environment of the thruster. Any sufficiently small probe will melt, and available optical plasma diagnostics do not have the sensitivity and/or spatial resolution to resolve the sheath region. The goal of the current work is to experimentally characterize plasma sheaths xxvi in a low-density plasma that yields centimeter-thick sheath layers. By generating thick sheaths, spatially-resolved data can obtained using electrostatic probes. The investigation focuses on the effects of electron emission from the wall and several factors that influence it, including wall material, wall temperature, wall surface roughness and topology, as well as the scaling of sheaths from the low-density plasma environment towards thruster conditions. The effects of electron emission and wall material are found to agree with classical fluid and kinetic theory extended from literature. In conditions of very strong emission from the wall, evidence is found for a full transition in sheath polarities rather than a non-monotonic structure. Wall temperature is observed to have no effect on the sheath over boron nitride walls independent of outgassing on initial heat-up, for sub-thermionic temperatures. Wall roughness is observed to postpone the effects of electron emission to higher plasma temperatures, indicating that the rough wall impairs the wall’s overall capacity to emit electrons. Reductions in electron yield are not inconsistent with a diffuse-emission geometric trapping model. Collectively, the experimental data provide an improved grounding for thruster modeling and design.Current state-of-the-art plasma thrusters are limited in power density and thrust density by power losses to plasma-facing walls and electrodes. In the case of Hall effect thrusters, power deposition to the discharge channel walls and anode negatively impact the efficiency of the thruster and limit the attainable power density and thrust density. The current work aims to recreate thruster-relevant wall-interaction physics in a quiescent plasma and investigate them using electrostatic probes, in order to inform the development of the next generation of high-power-density / high-thrust-density propulsion devices. Thruster plasma-wall interactions are complicated by the occurrence of the plasma sheath, a thin boundary layer that forms between a plasma and its bounding wall where electrostatic forces dominate. Sheaths have been recognized since the seminal work of Langmuir in the early 1900’s, and the theory of sheaths has been greatly developed to the present day. The theories are scalable across a wide range of plasma parameters, but due to the difficulty of obtaining experimental measurements of plasma properties in the sheath region, there is little experimental data available to directly support the theoretical development. Sheaths are difficult to measure in situ in thrusters due to the small physical length scale of the sheath (order of micrometers in thruster plasmas) and the harsh plasma environment of the thruster. Any sufficiently small probe will melt, and available optical plasma diagnostics do not have the sensitivity and/or spatial resolution to resolve the sheath region. The goal of the current work is to experimentally characterize plasma sheaths xxvi in a low-density plasma that yields centimeter-thick sheath layers. By generating thick sheaths, spatially-resolved data can obtained using electrostatic probes. The investigation focuses on the effects of electron emission from the wall and several factors that influence it, including wall material, wall temperature, wall surface roughness and topology, as well as the scaling of sheaths from the low-density plasma environment towards thruster conditions. The effects of electron emission and wall material are found to agree with classical fluid and kinetic theory extended from literature. In conditions of very strong emission from the wall, evidence is found for a full transition in sheath polarities rather than a non-monotonic structure. Wall temperature is observed to have no effect on the sheath over boron nitride walls independent of outgassing on initial heat-up, for sub-thermionic temperatures. Wall roughness is observed to postpone the effects of electron emission to higher plasma temperatures, indicating that the rough wall impairs the wall’s overall capacity to emit electrons. Reductions in electron yield are not inconsistent with a diffuse-emission geometric trapping model. Collectively, the experimental data provide an improved grounding for thruster modeling and design.
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Books on the topic "PLASMA SHEATH"

1

Stangeby, P. C. The plasma sheath. [S.l.]: [s.n.], 1986.

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Riggs, John Forrest. Anode sheath contributions in plasma thrusters. Monterey, Calif: Naval Postgraduate School, 1994.

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Brown, George Scott. Exploring plasma sheath solutions for planar and cylindrical anodes. Monterey, Calif: Naval Postgraduate School, 1991.

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Hayes, John Richard. Validation of a plasma sheath model for use in RF sputtering systems. [s.l: The Author], 2003.

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Lai, Shu T. Spacecraft sheath modification during beam ejection. Hanscom AFB, MA: Space Physics Division, Air Force Geophysics Laboratory, 1985.

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Lai, Shu T. Spacecraft sheath modification during beam ejection. Hanscom AFB, MA: Space Physics Division, Air Force Geophysics Laboratory, 1985.

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Lai, Shu T. Spacecraft sheath modification during beam ejection. Hanscom AFB, MA: Space Physics Division, Air Force Geophysics Laboratory, 1985.

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V, Chugunov I͡U︡, ed. Antenny v plazme. Nizhniĭ Novgorod: Akademii͡a︡ nauk SSSR, In-t prikladnoĭ fiziki, 1991.

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Carruth, M. R. Surface voltage gradient role in high voltage solar array/plasma interactions. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1985.

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Hillard, G. Barry. Plasma chamber testing of APSA coupons for the SAMPIE flight experiment. [Washington, DC: National Aeronautics and Space Administration, 1993.

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Book chapters on the topic "PLASMA SHEATH"

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Militello, Fulvio. "Sheath Physics." In Boundary Plasma Physics, 89–143. Cham: Springer International Publishing, 2022. http://dx.doi.org/10.1007/978-3-031-17339-4_3.

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Stangeby, Peter C. "The Plasma Sheath." In Physics of Plasma-Wall Interactions in Controlled Fusion, 41–97. Boston, MA: Springer US, 1986. http://dx.doi.org/10.1007/978-1-4757-0067-1_3.

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Krasheninnikov, Sergei, Andrei Smolyakov, and Andrei Kukushkin. "Sheath Physics." In Springer Series in Plasma Science and Technology, 73–87. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-49594-7_4.

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Favre, M., P. Silva, H. Chuaqui, E. Wyndham, and P. Choi. "Current Sheath Studies in A Small Plasma Focus Operating in Hydrogen-Argon Mixtures." In Plasma Physics, 485–90. Dordrecht: Springer Netherlands, 1998. http://dx.doi.org/10.1007/978-94-011-4758-3_57.

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Gupta, G. S. "Fibrous Sheath, Dense Fibers, and Plasma Membrane of Sperm." In Proteomics of Spermatogenesis, 695–720. Boston, MA: Springer US, 2005. http://dx.doi.org/10.1007/0-387-27655-6_29.

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Chodura, Roland. "Plasma Flow in the Sheath and the Presheath of a Scrape-Off Layer." In Physics of Plasma-Wall Interactions in Controlled Fusion, 99–134. Boston, MA: Springer US, 1986. http://dx.doi.org/10.1007/978-1-4757-0067-1_4.

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Deka, K., R. Paul, G. Sharma, S. Adhikari, R. Moulick, S. S. Kausik, and B. K. Saikia. "Study of Plasma Sheath in the Presence of Dust Particles in an Inhomogeneous Magnetic Field." In Springer Proceedings in Physics, 363–73. Singapore: Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-16-5141-0_39.

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Speiser, T. W. "Plasma sheet theories." In Modeling Magnetospheric Plasma, 277–88. Washington, D. C.: American Geophysical Union, 1988. http://dx.doi.org/10.1029/gm044p0277.

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Lotko, W., and C. G. Schultz. "Internal shear layers in auroral dynamics." In Modeling Magnetospheric Plasma, 121–32. Washington, D. C.: American Geophysical Union, 1988. http://dx.doi.org/10.1029/gm044p0121.

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Parks, George K. "Boundaries and Current Sheets." In Characterizing Space Plasmas, 191–234. Cham: Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-90041-4_5.

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Conference papers on the topic "PLASMA SHEATH"

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Zhykharsky, A. V., and B. I. Yudin. "Transition sheath "plasma-wall"." In 1998 4th International Conference on Actual Problems of Electronic Instrument Engineering Proceedings. APEIE-98. IEEE, 1998. http://dx.doi.org/10.1109/apeie.1998.768910.

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Annaratone, B. M. "Diagnosis of a plasma in plasma-sheath resonance." In IEE Colloquium on Measurement and Plasma. IEE, 1997. http://dx.doi.org/10.1049/ic:19970513.

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Rezaee, M. R., A. R. Niknam, H. Ghomi, and H. Latifi. "Magnetized plasma sheath dynamics in plasma source ion implantation." In 2008 IEEE 35th International Conference on Plasma Science (ICOPS). IEEE, 2008. http://dx.doi.org/10.1109/plasma.2008.4590622.

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Xing Xing Wang, Xing Xing Wang, and Tsin Chi Yang Tsin Chi Yang. "Structure of plasma sheath in a plasma focus device." In 1990 Plasma Science IEEE Conference Record - Abstracts. IEEE, 1990. http://dx.doi.org/10.1109/plasma.1990.110793.

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Zhang, Quan-Zhi, Jing-Yu Sun, Yuan-Hong Song, and You-Nian Wang. "Non-Linear Sheath Oscillation Mechanism in Symmetric Capacitively Coupled Plasma Sheaths." In 2020 IEEE International Conference on Plasma Science (ICOPS). IEEE, 2020. http://dx.doi.org/10.1109/icops37625.2020.9717820.

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BIBLARZ, OSCAR, and JOHN RIGGS. "Anode sheath contributions in plasma thrusters." In 29th Joint Propulsion Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-2495.

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Balmain, K. G. "Sheath Waves on Conductors in Plasma." In International Conference on Plasma Sciences (ICOPS). IEEE, 1993. http://dx.doi.org/10.1109/plasma.1993.593045.

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Chalise, R., and R. Khanal. "Self-Consistant 1D3V Kinetic Trajectory Simulation Model of Magnetized Plasma Sheath Sheath." In 2018 IEEE International Conference on Plasma Science (ICOPS). IEEE, 2018. http://dx.doi.org/10.1109/icops35962.2018.9575673.

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Langendorf, S., and M. Walker. "Effects of surface roughness on plasma sheath." In 2014 IEEE 41st International Conference on Plasma Sciences (ICOPS) held with 2014 IEEE International Conference on High-Power Particle Beams (BEAMS). IEEE, 2014. http://dx.doi.org/10.1109/plasma.2014.7012716.

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Yang, Min, Xiaoping Li, Yanming Liu, Lei Shi, and Xiaolin Wang. "Characteristic of time-varying plasma sheath channel." In 2012 10th International Symposium on Antennas, Propagation & EM Theory (ISAPE - 2012). IEEE, 2012. http://dx.doi.org/10.1109/isape.2012.6408836.

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Reports on the topic "PLASMA SHEATH"

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Birdsall, Charles K. Plasma-Sheath-Surface Dynamics. Fort Belvoir, VA: Defense Technical Information Center, September 1990. http://dx.doi.org/10.21236/ada226086.

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Riley, M. E. Unified model of the rf plasma sheath. Office of Scientific and Technical Information (OSTI), May 1995. http://dx.doi.org/10.2172/70709.

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Xu, X. Q., G. DiPeso, V. Vahedi, and C. K. Birdsall. Theory and simulation of plasma sheath waves. Office of Scientific and Technical Information (OSTI), December 1992. http://dx.doi.org/10.2172/10186872.

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Whittum, David H. Electron-Hose Instability in an Annular Plasma Sheath. Office of Scientific and Technical Information (OSTI), July 1999. http://dx.doi.org/10.2172/9904.

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Abe Fetterman, Yevgeny Raitses, and Michael Keidar. Anode Sheath Switching in a Carbon Nanotube Arc Plasma. Office of Scientific and Technical Information (OSTI), April 2008. http://dx.doi.org/10.2172/960288.

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Kaganovich, Igor D. How to Patch Active Plasma and Collisionless Sheath: Practical Guide. Office of Scientific and Technical Information (OSTI), August 2002. http://dx.doi.org/10.2172/809821.

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Riley, M. E. Unified model of the rf plasma sheath: Part 2, Asymptotic connection formulae. Office of Scientific and Technical Information (OSTI), August 1996. http://dx.doi.org/10.2172/274143.

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M.C. Campanell, A. Khrabrov and I. Kaganovich. General Cause of Sheath Instability Identified for Low Collisionality Plasma in Devices with Secondary Electron Emission. Office of Scientific and Technical Information (OSTI), May 2012. http://dx.doi.org/10.2172/1062660.

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Sydorenko, D., A. Smolyakov, I. Kaganovich, and Y. Raitses. Plasma-Sheath Instability in Hall Thrusters Due to Periodic Modulation of the Energy of Secondary Electrons in Cyclotron Motion. Office of Scientific and Technical Information (OSTI), April 2008. http://dx.doi.org/10.2172/959391.

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Xiao, H., R. D. Hazeltine, and R. Carrera. Self-consistent radial sheath in ignited plasmas. Office of Scientific and Technical Information (OSTI), November 1991. http://dx.doi.org/10.2172/10107814.

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