2,239 research outputs found

    The blue lady - A case report

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    Indian Journal of Anaesthesia506435-438Indi

    Capturing an Evader in a Polygonal Environment With Obstacles

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    We study a pursuit-evasion game in which one or more cops try to capture a robber by moving onto a robber's current location. All players have equal maximum velocities. We show that three cops can capture the robber in any polygonal environment which can contain any finite number of holes.Bhadauria, Deepak; Gosse, Shaun; Pipp, Joseph. (2010). Capturing an Evader in a Polygonal Environment With Obstacles. Retrieved from the University Digital Conservancy, https://hdl.handle.net/11299/215845

    Non-respiratory functions of the lung

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    10.1093/bjaceaccp/mks060Continuing Education in Anaesthesia Critical Care & Pain13398-10

    My Name Is Deepak

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    This chapter looks at the author's responses to being given a nickname by his co-workers: Tupac. They do it in a friendly manner, but the author doesn’t understand the connection with the American rapper. It makes him think about who he is, his identity, and how people see him in his adopted country.</p

    Sideffective - system to mine patient reviews: sentiment analysis

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    Sideffective is the system to crawl, rank and analyze patient testimonials about side ffeects from common medications. Since the wealth of any mining model is the Data corpus, the data collection phase involved extensive crawling of massive medical websites comprised of user forums from the internet. Subsequently, the raw files were subjected to certain site-specific parsing routines, yielding outputs conforming to a well-defined data model. Currently, the system holds close to 400,000 user testimonials pertaining to more than 2500 drugs/medicines. Sideffective aims at gathering and aggregating this wealth of information, build useful associations and present interesting observations and numeric validations, all in a user-friendly interface. The important issues that we have tried to tackle are: Extracting side effects without relying on pre-built lists, aggregating distribution of different side effect for a give drug, site-specific search, ranking and determining the negativity of reviews. The system has been jointly built by Deepak Yalamanchi and Sangeetha Rajagopalan under the guidance of Prof. Tomasz Imielinski. This thesis focuses mainly on Sentiment Analysis of patient reviews. While most existing sentiment analysis systems are predicated by POS (parts of speech) tagging or Bayesian sentiment analysis methods, the same cannot be applied to medical reviews as they generally carry a negative flavor in them. We thereby approached the problem by identifying the features in the sentence and calibrating the sentiment on a Negativity Meter based on their relation to sentiment words. A feature, as defined for the purpose of this thesis, can be a medicine, a side effect or a symptom. The sentiment of each feature is determined by the aggregate of all its polarities with respect to each sentiment word, where the polarity is determined by an inverse relation to the distance of the feature from the sentiment word. Each sentence is then evaluated by the cumulative polarity of all the features contained in it. Sentiment of a review is determined by individually determining the sentiment of each sentence and then getting a weighted sum score of all the sentences in the review. The accuracy of a sentiment analysis system is, in principle, how well it agrees with human judgments. Experimental results, involving human reviewers (extracted from site: www.askapatient.com) and correlating them back to the negativity rating of each review yield conclusive results, demonstrating the effectiveness of the technique. We have also implemented a customized Lucene search on the data using a multi-review summarization approach and a ranking scheme based on the feature-list. Ranking priority is given to the review that has the largest feature list size.M.S.Includes bibliographical referencesby Deepak Yalamanch

    Macroeconomics and Growth Policies

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    This United Nations Background Note on Macroeconomics and Growth provides practical guidance on how to operationalize alternative equitable and employment-generating macroeconomic and growth policies in National Development Strategies. This Policy Note has been developed in cooperation with UN agencies, and has been officially reviewed by distinguished academics/ development specialists such as Jose Antonio Ocampo, Jomo K.S. and Nobel Laureate Joseph Stiglitz.macroeconomics, growth, development planning

    On the balance between the tonal and broadband noise of uninstalled propellers

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    This paper provides a preliminary theoretical investigation of the balance between rotor alone tonal and broadband noise. First, using well-published theory, the different source mechanisms for tonal and broadband noise are discussed and presented. Then, using these theoretical results, an extensive parametric study has been performed in which the propeller thrust, diameter and blade solidity have been maintained constant, but the blade tip speed and blade numbers have been allowed to vary. In order to account for the variations in noise against directivity and, simultaneously, across the audible frequency range, the data are presented as Overall Sound Pressure Levels (OASPLs) and as Overall Acoustic Sound Power Level (OSWLs) integrated over the frequency range. Using these collapsed data metrics, it is found that the tonal noise dominates at low frequency and/or low tip speeds but that broadband noise is the major contributor at high-frequencies and low tip speeds. The results show a clear distinction between the regions dominated by tonal contributions and those dominated by broadband contributions. These results are discussed and related to the different tone and broadband source physical mechanisms. In addition to the primary parametric study, the paper also investigates, separately, the effects of changes in blade chord and propeller thrust. The studies presented in this paper are intended to serve as noise guidelines for propeller preliminary design

    sj-docx-1-cpj-10.1177_00099228231200405 – Supplemental material for Association Between Child Sugary Drink Consumption and Serum Lipid Levels in Electronic Health Records

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    Supplemental material, sj-docx-1-cpj-10.1177_00099228231200405 for Association Between Child Sugary Drink Consumption and Serum Lipid Levels in Electronic Health Records by Ankitha Iyer, Fang-Chi Hsu, Alex Bonnecaze, Joseph A. Skelton, Deepak Palakshappa and Kristina H. Lewis in Clinical Pediatrics</p

    Analytical investigation of propeller-wing interaction noise

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    This paper investigates the noise generated by propeller-wing configuration at take-off condition with the propeller mounted upstream. This study makes use of various axisymmetric noise models developed for contra-rotating propellers to estimate the noise generated by propeller-wing configuration and later integrate them to estimate total noise. First, using well-published theory, rotor-alone (loading, thickness, and self-noise) and interaction noise sources (viscous-wake, potential field, tip-vortex) including tonal and broadband components are estimated. Later, a systematic parametric study is carried out by changing the blade number and tip Mach, while maintaining the propeller thrust and blade solidity. The noise generated is represented by Overall Acoustic Sound Power Level (OSWLs), which is an integrated value over the emission angles and frequency range, in a matrix form for the range of blade number and tip Mach. This matrix shows the regions dominated by rotor-alone and interaction noise and found that the noise characteristics of a rotor in uninstalled conditions (rotor-alone) are significantly altered due to the presence of a wing (installed condition). Further, it is found that the balance between these regions shifts with the variation in separation distance between the propeller and the wing. These results are further discussed with the individual interaction noise source mechanism and their dominance at various blade numbers, tip Mach, and separation distances. In addition, the non-axisymmetric viscous-wake interaction noise is investigated for even and odd numbers of blades and found that viscous-wake interaction noise has considerable directivity in the azimuthal direction. The results presented in the study are preliminary findings of propeller-wing noise, however, it gives give a quantitative picture of the behaviour of various noise sources and their balance with respect to geometric and operating parameters. This study will help to understand the dominant noise sources involved in propeller-wing configuration and will provide a quick guide for designing a low-noise configuration
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