Academic literature on the topic 'Dual-stream'

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Journal articles on the topic "Dual-stream"

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Wang, Xi, Malcolm Crowe, and Colin Fyfe. "Dual stream data exploration." International Journal of Data Mining, Modelling and Management 4, no. 2 (2012): 188. http://dx.doi.org/10.1504/ijdmmm.2012.046810.

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Loui, Psyche. "A Dual-Stream Neuroanatomy of Singing." Music Perception 32, no. 3 (February 1, 2015): 232–41. http://dx.doi.org/10.1525/mp.2015.32.3.232.

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Singing requires effortless and efficient use of auditory and motor systems that center around the perception and production of the human voice. Although perception and production are usually tightly coupled functions, occasional mismatches between the two systems inform us of dissociable pathways in the brain systems that enable singing. Here I review the literature on perception and production in the auditory modality, and propose a dual-stream neuroanatomical model that subserves singing. I will discuss studies surrounding the neural functions of feedforward, feedback, and efference systems that control vocal monitoring, as well as the white matter pathways that connect frontal and temporal regions that are involved in perception and production. I will also consider disruptions of the perception-production network that are evident in tone-deaf individuals and poor pitch singers. Finally, by comparing expert singers against other musicians and nonmusicians, I will evaluate the possibility that singing training might offer rehabilitation from these disruptions through neuroplasticity of the perception-production network. Taken together, the best available evidence supports a model of dorsal and ventral pathways in auditory-motor integration that enables singing and is shared with language, music, speech, and human interactions in the auditory environment.
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Wu, Xuecheng, Qimeng Lv, Yingchun Wu, Can Li, and Kefa Cen. "Dual-stream of monodisperse droplet generator." Chemical Engineering Science 223 (September 2020): 115645. http://dx.doi.org/10.1016/j.ces.2020.115645.

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Holländer, Antje, Michael C. Corballis, and Jeff P. Hamm. "Visual-field asymmetry in dual-stream RSVP." Neuropsychologia 43, no. 1 (January 2005): 35–40. http://dx.doi.org/10.1016/j.neuropsychologia.2004.06.006.

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Murakami, Erina, and Dimitri Papamoschou. "Mean Flow Development in Dual-Stream Compressible Jets." AIAA Journal 40, no. 6 (June 2002): 1131–38. http://dx.doi.org/10.2514/2.1762.

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Viswanathan, K. "True Farfield for Dual-Stream Jet Noise Measurements." AIAA Journal 49, no. 2 (February 2011): 443–47. http://dx.doi.org/10.2514/1.j050771.

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VISWANATHAN, K. "Parametric study of noise from dual-stream nozzles." Journal of Fluid Mechanics 521 (December 25, 2004): 35–68. http://dx.doi.org/10.1017/s0022112004000813.

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Tam, Christopher K. W., N. N. Pastouchenko, and K. Viswanathan. "Broadband shock-cell noise from dual stream jets." Journal of Sound and Vibration 324, no. 3-5 (July 2009): 861–91. http://dx.doi.org/10.1016/j.jsv.2009.02.012.

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Upton, Emily, and Thomas M. H. Hope. "Moving beyond the dual stream account of language." Brain 143, no. 8 (August 1, 2020): 2336–38. http://dx.doi.org/10.1093/brain/awaa197.

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Xu, Ning, An-An Liu, Yongkang Wong, Yongdong Zhang, Weizhi Nie, Yuting Su, and Mohan Kankanhalli. "Dual-Stream Recurrent Neural Network for Video Captioning." IEEE Transactions on Circuits and Systems for Video Technology 29, no. 8 (August 2019): 2482–93. http://dx.doi.org/10.1109/tcsvt.2018.2867286.

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Dissertations / Theses on the topic "Dual-stream"

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Speechley, William Jonathan. "Dual-stream modulation failure, cognitive biases and delusions in schizophrenia." Thesis, University of British Columbia, 2012. http://hdl.handle.net/2429/42246.

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Recent cognitive research has made important contributions to our understanding of delusions, but there have been few attempts to generate a general model that address both delusion formation and maintenance, with a focus on the mechanisms that may underlie the cognitive characteristics of delusions. This thesis describes studies replicating and extending our understanding of two previously identified cognitive biases, and then outlines the development and initial testing of a new model of delusions. The Dual-Stream Modulation Failure (DSMF) model suggests that delusions are the result of an imbalance between two streams of reasoning: Stream 1, which is automatic and intuitive, and Stream 2, which is slower and more deliberative. The degree to which each stream is favoured in a given situation may depend on two modulators: conflict and emotion. Cognitive conflict may cause an individual to consider the available evidence more carefully, while emotional salience may favour reflexive, non-deliberative processing. In schizophrenia, conflict modulation failure (CMF) and/or accentuated emotional modulation (AEM) may result in an under-recruitment of Stream 2 processing and over-reliance on Stream 1, increasing the likelihood that erroneous interpretations will form and be maintained. The first study employs a variation of a classic probabilistic reasoning paradigm to provide new insights into to the jumping-to-conclusions and over-adjustment biases. The second study describes the first multivariate analysis of bias against disconfirmatory evidence (BADE) data using all available information from the task to aid interpretation of the cognitive underpinnings of the evidence integration necessary in the BADE task. The third and fourth studies investigate the DSMF model of delusions using a conditional reasoning paradigm that places content believability in conflict with logical validity. Support is provided for CMF, with the schizophrenia group showing a greater drop in performance and a significantly smaller increase in activity in areas of the brain associated with conflict and deliberative processing for conflict compared to non-conflict stimuli. No evidence was found for AEM, suggesting that future DSMF research may either need to make adjustments to the experimental paradigm or to the model itself.
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Almeida, Odenir de. "Aeroacoustics of dual-stream jets with application to turbofan engines." Instituto Tecnológico de Aeronáutica, 2009. http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=805.

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A Computational Aeroacoustics (CAA) and a novel semi-empirical model is developed for predicting the noise generated by the jet flow through dual stream (coaxial) nozzles, as found in modern turbofan engines. The acoustic source model was developed in a 2D and 3D framework, based on the Lilley's Equations, following the traditional MGBK method from NASA Langley Research Center. The semi-empirical model was based on the Four-Source model from the Institute of Sound and Vibration (ISVR). This suite of methodologies provided a mean of investigating the mechanisms of noise generation and propagation of subsonic coaxial jet flows, as well as the noise prediction at different operating conditions. The work done contributed to the development and improvement of a numerical tool for jet noise prediction of dual-stream exhaust systems, commonly employed in turbofan engines. Such research also subsidies the improvement of semi-empirical methods used in the Center of Reference in Gas Turbine (ITA) for the noise prediction of turbofans in all operating conditions.
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Schlesser, Benjamin Joseph. "Development and evaluation of a single pass, dual stream corn stover harvester." [Ames, Iowa : Iowa State University], 2007. http://gateway.proquest.com/openurl?url_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:dissertation&res_dat=xri:pqdiss&rft_dat=xri:pqdiss:1461386.

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Pérez, Arroyo Carlos. "Large eddy simulations of a dual-stream jet with shockcells and noise emission analysis." Thesis, Toulouse, INPT, 2016. http://www.theses.fr/2016INPT0093/document.

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Cette thèse fait référence au bruit de choc généré par des jets sousdétendus simple ou en configuration co-axial. Le bruit de choc est généré par l'interaction entre les structures turbulentes de la couche de cisaillement et le réseaux de cellules de choc développé dans le cône potentiel du jet. Afin d'étudier le bruit choc, simulations à grandes échelles adaptés pour l'aéro-acoustique sont effectué avec des schémas d'ordre élevé qui permet une approche nondissipative et non-dispersive. Les résultats sont analysés et comparés avec des résultats expérimentaux. Notamment, une filtrage hydrodynamique et acoustique est réalisé dans le champ proche pour analyser les modes azimutaux acoustiques et hydrodynamiques. En outre, un analyse basé sur la transformé en ondelettes est mis en oeuvre pour identifier les caractéristiques acoustiques et hydrodynamiques importants des jets supersoniques
This thesis deals with the shock-cell noise generated by under-expanded supersonic jets in single- and dualstream configurations. Shock-cell noise is generated by the interaction between the turbulent structures of the shear-layer and the shock-cell system developed in the potential core of the jet. In order to study shock-cell noise, large eddy simulations adapted to aeroacoustics are carried out using high-order compact schemes that allow for a non-dissipative nondispersive approach. The results are analyzed and compared to experimental results. In particular, an acoustic-hydrodynamic filtering is carried out in the near field in order to analyze the acoustic and hydrodynamic azimuthal modes. Moreover, a wavelet-based analysis is implemented in order to identify the relevant acoustic and hydrodynamic features of the supersonic jets
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Ansaldi, Tobias. "Compressible single and dual stream jet stability and adjoint-based sensitivity analysis in relationship with aeroacoustics." Phd thesis, Toulouse, INPT, 2016. http://oatao.univ-toulouse.fr/17505/13/Ansaldi_Tobias.pdf.

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This thesis leads to a better knowledge of the physic and of the control of acoustic radiation in turbulent single and dual-stream jets.It is known that jet noise is produced by the turbulence present in the jet that can be separated in large coherent structures and fine structures. It is also concluded that these large-scale coherent structures are the instability waves of the jet and can be modelled as the flow field generated by the evolution of instability waves in a given turbulent jet. The growth rate and the streamwise wavenumber of a disturbance with a fixed frequency and azimuthal wavenumber are obtained by solving the non-local approach called Parabolized Stability Equations (PSE). Typically the Kelvin-Helmholtz instability owes its origin into the shear layer of the flow and, moreover, the inflection points of the mean velocity profile has a crucial importance in the instability of such a flow. The problem is more complex in case of imperfectly expanded jet where shock-cells manifest inside the jet and strongly interaction with the instability waves has been observed. Several configurations are tested in this thesis, from a subsonic incompressible case to the dual-stream underexpanded supersonic jet obtained by solving Large Eddy Simulations LES (CERFACS). The acoustic far-field is determined by the Ffowcs-Williams-Hawkings acoustic analogy. Then a sensitivity analysis of the jet with respect to external forcing acting in a localized region of the flow are investigated by solving the adjoint PSE equations. High sensitivity appeared in the shear-layer of the flow showing, also, a high dependency in the streamwise and radial direction. In the case of dual-stream jet the propagation of the instability in the inner and outer shear layer should be taken into account. This configuration leads to two different distinct Klevin-Helmholtz modes that are computed separately. The highest sensitivity is determined in the exit of the nozzle outside of the potential core of the jet. In addition, comparison between sensitivity computed by adjoint equations and Uncertainty Quantification (UQ) methods has been done, in the case of a single-stream jet, showing a link between these two methods for small variations of the input parameters. This result leads to the application of a lower cost tool for mathematical analysis of complex problem of industrial interest. This work and in particular the sensitivity theory investigated in this thesis contribute to a development of a new noise control strategy for aircraft jet.
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Nakae, Takuro. "Connectivity Gradient in the Human Left Inferior Frontal Gyrus: Intraoperative Cortico-Cortical Evoked Potential Study." Kyoto University, 2020. http://hdl.handle.net/2433/254513.

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Mustafa, Mansoor. "Investigation into Offset Streams for Jet Noise Reduction." The Ohio State University, 2015. http://rave.ohiolink.edu/etdc/view?acc_num=osu1437477139.

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Léon, Olivier. "Étude du rayonnement acoustique d'instabilités hydrodynamiques de jets double-flux par les équations de stabilité parabolisées (PSE)." Phd thesis, Toulouse, INPT, 2012. http://oatao.univ-toulouse.fr/9138/1/leon_partie_1_sur_2.pdf.

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Dans le but de réduire le bruit de jet, source principale de nuisance sonore au décollage d'un avion, une compréhension fine des mécanismes aéroacoustiques mis en jeu est nécessaire. Les structures cohérentes de grande échelle se développant dans la couche de mélange d'un jet semblent responsables d'une part importante du bruit observé en champ lointain, surtout dans les basses fréquences. Une approche permettant d'étudier ces structures turbulentes est fournie par la théorie de stabilité, notamment au moyen des équations de stabilité parabolisées (PSE). L'étude de ces ondes d'instabilité est alors complémentaire d'autres approches (LES ou expériences), puisqu'elle permet de mettre en évidence la nature et la dynamique de ces structures, également présentes dans les résultats de simulations ou de mesures. Au cours de ces travaux de thèse, nous nous sommes intéressés aux structures cohérentes se développant dans des jets à double flux étudiés au cours du projet européen CoJeN (Coaxial Jet Noise). En particulier, nous avons exploité une base de données issues de mesures de fluctuations de pression réalisées en champ proche et en champ lointain de ces jets. Nous avons alors pu comparer les résultats de notre modélisation PSE à ces mesures en périphérie immédiate du jet, confirmant ainsi la pertinence d’un tel modèle, même dans des configurations aussi complexes. De plus, le calcul du rayonnement acoustique en champ lointain engendré par les fluctuations de pression modélisées nous a permis de faire des comparaisons directes avec les niveaux et les directivités mesurés. Nous avons ainsi pu mettre en évidence quantitativement la contribution de ces structures turbulentes de grande échelle au bruit total rayonné par le jet.
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ZHEN, XI-GI, and 鄭錫齊. "Design of the dual-alu CRISC and its dual-stream instruction execution." Thesis, 1988. http://ndltd.ncl.edu.tw/handle/49095638536599542283.

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碩士
國立交通大學
電子研究所
76
CRISC(Reduced Instrction Set Computer for The C Language )是一個可提共一 般C 語言功能的32位元有限指令集計算機。它是一個基於RISC精神,並包含多個功 能運算單元的中央處理器。雙運算器可用於時執行多個指令。 本論文中首先趼究先RISC的精神和如何提高並行執行的效率。配合計算機架構的設計 與考慮,提出一個包含隱藏式記憶體在處理機內的計算機架構,而且最後的微架構也 會被提出。本文中同時將探討一些提高CRISC 性能的技巧。除此以外,正式的 CRISC 性能評估也會在本文中提出。
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Pérez, Arroyo Carlos. "Large eddy simulations of a dual-stream jet with shockcells and noise emission analysis." Phd thesis, 2016. http://oatao.univ-toulouse.fr/16684/13/PerezArroyo_1.pdf.

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This thesis deals with the shock-cell noise generated by under-expanded supersonic jets in single- and dualstream configurations. Shock-cell noise is generated by the interaction between the turbulent structures of the shear-layer and the shock-cell system developed in the potential core of the jet. In order to study shock-cell noise, large eddy simulations adapted to aeroacoustics are carried out using high-order compact schemes that allow for a non-dissipative nondispersive approach. The results are analyzed and compared to experimental results. In particular, an acoustic-hydrodynamic filtering is carried out in the near field in order to analyze the acoustic and hydrodynamic azimuthal modes. Moreover, a wavelet-based analysis is implemented in order to identify the relevant acoustic and hydrodynamic features of the supersonic jets.
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Books on the topic "Dual-stream"

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Glahn, U. Von. Plume characteristics of single-stream and dual-flow conventional and inverted-profile nozzles at equal thrust. [Washington, DC]: National Aeronautics and Space Administration, 1986.

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Carpenter, Thomas. Evaluation of dual flow, thrust vector nozzles with exhaust stream impingement: Semi-annual progress report 6/92-12/92, NASA-Ames grant number NAG 2-778. San Luis Obispo, Calif: California Polytechnic State University, 1992.

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F, Brausch J., Majjigi R. K, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Free jet feasibility study of a thermal acoustic shield concept for AST/VCE application: Dual stream nozzles. [Washington, D.C.?]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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Evaluation of dual flow, thrust vector nozzles with exhaust stream impingement: Final technical report 10/90 - 7/91, NASA-Ames grant number NAG 2-778. San Luis Obispo, Calif: California Polytechnic State University, 1991.

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United States. National Aeronautics and Space Administration., ed. Evaluation of dual flow, thrust vector nozzles with exhaust stream impingement: Final technical report 10/90 - 7/91, NASA-Ames grant number NAG 2-778. San Luis Obispo, Calif: California Polytechnic State University, 1991.

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United States. National Aeronautics and Space Administration., ed. Evaluation of dual flow, thrust vector nozzles with exhaust stream impingement: Semi-annual progress report 6/92-12/92, NASA-Ames grant number NAG 2-778. San Luis Obispo, Calif: California Polytechnic State University, 1992.

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F, Spina Eric, and United States. National Aeronautics and Space Administration., eds. The noise reduction potential of dual-stream coaxial rectangular improperly expanded jet flows: Final grant report, NASA Langley grant NAG-1-1240, covering the period March 1991 to March 1993. [Washington, DC: National Aeronautics and Space Administration, 1995.

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The noise reduction potential of dual-stream coaxial rectangular improperly expanded jet flows: Final grant report, NASA Langley grant NAG-1-1240, covering the period March 1991 to March 1993. [Washington, DC: National Aeronautics and Space Administration, 1995.

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Lewis, Marc D. The Development of Emotion Regulation. Edited by Philip David Zelazo. Oxford University Press, 2013. http://dx.doi.org/10.1093/oxfordhb/9780199958474.013.0004.

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This chapter examines the relation between normative advances and emerging individual differences in emotion regulation (ER), using principles from developmental cognitive neuroscience to integrate these seemingly disparate processes. Like several other theorists, I view corticolimbic development as a self-organizing stream of synaptic alterations, driven by experience rather than biologically prespecified. This conceptualization helps resolve ambiguities that appear when we try, but consistently fail, to neatly parse individual differences and developmental differences. At the neural level, increasingly specific patterns of synaptic activation converge in response to (or in anticipation of) recurrent emotions, creating synaptic networks that link multiple regions. These networks regulate emotions (in real time). But they also stabilize and consolidate with repetition, thus giving rise tohabitsthat are the hallmark of individual development. These configurations are progressively sculpted through individual learning experiences, but they also become increasingly effective with use, thereby expressing both individual trajectories and normative advances as they develop. In sum, experience-driven synaptic changes create a repertoire of individual solutions to universal challenges, shared among members of a culture or society. This description casts individual differences and age-related advances as dual facets of a unitary developmental process.
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Book chapters on the topic "Dual-stream"

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Fyfe, Colin. "Dual Stream Artificial Neural Networks." In Lecture Notes in Computer Science, 16–17. Berlin, Heidelberg: Springer Berlin Heidelberg, 2004. http://dx.doi.org/10.1007/978-3-540-30132-5_6.

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Hu, Xiaojun, Miao Kang, Weilin Huang, Matthew R. Scott, Roland Wiest, and Mauricio Reyes. "Dual-Stream Pyramid Registration Network." In Lecture Notes in Computer Science, 382–90. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-32245-8_43.

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Khan, Aqib, Praneeta B. Sachan, Akhil K. Mathews, Shivam Verma, Priyanka Hankare, Rakesh Kumar, and Sanjay Kumar. "Interfacial Waves in Dual Stream Granular Flows." In Lecture Notes in Mechanical Engineering, 453–58. Singapore: Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-15-5183-3_48.

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Müller, Egon, Timo Stock, and Rainer Schillig. "Dual Energy Signatures Enable Energy Value-Stream Mapping." In Advances in Sustainable and Competitive Manufacturing Systems, 1603–11. Heidelberg: Springer International Publishing, 2013. http://dx.doi.org/10.1007/978-3-319-00557-7_129.

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Ergüler, I., and E. Anarim. "A Clock-controlled Stream Cipher with Dual Mode." In Springer Proceedings in Physics, 343–52. Berlin, Heidelberg: Springer Berlin Heidelberg, 2006. http://dx.doi.org/10.1007/3-540-30636-6_38.

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Chandni, Rajat Khurana, and Alok Kumar Singh Kushwaha. "Delving Deeper with Dual-Stream CNN for Activity Recognition." In Lecture Notes in Electrical Engineering, 333–42. Singapore: Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-13-2685-1_32.

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Chen, Zhen, Xiaoqing Guo, Chen Yang, Bulat Ibragimov, and Yixuan Yuan. "Joint Spatial-Wavelet Dual-Stream Network for Super-Resolution." In Medical Image Computing and Computer Assisted Intervention – MICCAI 2020, 184–93. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-59722-1_18.

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Mendel, Florian, Tomislav Nad, and Martin Schläffer. "Collision Attacks on the Reduced Dual-Stream Hash Function RIPEMD-128." In Fast Software Encryption, 226–43. Berlin, Heidelberg: Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-34047-5_14.

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Lehmann, B., and J. Mante. "Turbulence Behaviour of Swirled Dual-Stream Nozzle Flows Without and With Combustion." In Notes on Numerical Fluid Mechanics (NNFM), 274–81. Wiesbaden: Vieweg+Teubner Verlag, 1999. http://dx.doi.org/10.1007/978-3-663-10901-3_36.

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Sheu, Tsang-Ling, and Yang-Shun Hsu. "Dual Mobile-IP Tunnels for Video Stream Splitting and Merging in Wireless Handoffs." In Lecture Notes in Computer Science, 15–26. Berlin, Heidelberg: Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-642-13315-2_2.

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Conference papers on the topic "Dual-stream"

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Wu, Song, Zhiyi Liu, Shadi Ibrahim, Lin Gu, Hai Jin, and Fei Chen. "Dual-Paradigm Stream Processing." In ICPP 2018: 47th International Conference on Parallel Processing. New York, NY, USA: ACM, 2018. http://dx.doi.org/10.1145/3225058.3225120.

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Rego, Leandro F., Francesco Avallone, Daniele Ragni, Damiano Casalino, and Wouter C. van der Velden. "Free-Stream Effects on Jet-Installation Noise of a Dual-Stream Engine." In 25th AIAA/CEAS Aeroacoustics Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2019. http://dx.doi.org/10.2514/6.2019-2491.

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Du, Baisheng, Xiaodong Xu, Zilong Zhang, and Xuchu Dai. "Precoder design for dual-stream MIMO multicasting." In 2013 International Conference on Wireless Communications and Signal Processing (WCSP). IEEE, 2013. http://dx.doi.org/10.1109/wcsp.2013.6677150.

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Khavaran, Abbas, and James Bridges. "Jet Noise Scaling in Dual Stream Nozzles." In 16th AIAA/CEAS Aeroacoustics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-3968.

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Sinha, Aniruddha, Datta V. Gaitonde, and Nikhil Sohoni. "Parabolized Stability Analysis of Dual-Stream Jets." In 22nd AIAA/CEAS Aeroacoustics Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2016. http://dx.doi.org/10.2514/6.2016-3057.

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Zhai, Shumin, Barton A. Smith, and Ted Selker. "Dual stream input for pointing and scrolling." In CHI '97 extended abstracts. New York, New York, USA: ACM Press, 1997. http://dx.doi.org/10.1145/1120212.1120406.

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Tam, Christopher, Nikolai Pastouchenko, and Krishna Viswanathan. "Broadband Shock-Cell Noise from Dual Stream Jets." In 14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference). Reston, Virigina: American Institute of Aeronautics and Astronautics, 2008. http://dx.doi.org/10.2514/6.2008-2833.

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Tam, Christopher, and Nikolai Pastouchenko. "Fine Scale Turbulence Noise from Dual Stream Jets." In 10th AIAA/CEAS Aeroacoustics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2004. http://dx.doi.org/10.2514/6.2004-2871.

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Georgiadis, Nicholas, and Dimitri Papamoschou. "Computational Investigations of High-Speed Dual Stream Jets." In 9th AIAA/CEAS Aeroacoustics Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2003. http://dx.doi.org/10.2514/6.2003-3311.

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Weng, Shuchen, Wenbo Li, Yi Zhang, and Siwei Lyu. "Dual-stream CNN for Structured Time Series Classification." In ICASSP 2019 - 2019 IEEE International Conference on Acoustics, Speech and Signal Processing (ICASSP). IEEE, 2019. http://dx.doi.org/10.1109/icassp.2019.8682410.

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