3 Pages

z hcr240 week2 speech (1)

Course: SCIENCE sci 241, Spring 2011
School: Arkansas Little Rock
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Word Count: 563

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Electronic Assignment: Medical Record Speech 1 Welcome to WritePoint, the automated review system that recognizes errors most commonly made by university students in academic essays. The system embeds comments into your paper and suggests possible changes in grammar and style. Please evaluate each comment carefully to ensure that the suggested change is appropriate for your paper, but remember that your...

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Course Hero has millions of student submitted documents similar to the one below including study guides, practice problems, reference materials, practice exams, textbook help and tutor support.
Electronic Assignment: Medical Record Speech 1 Welcome to WritePoint, the automated review system that recognizes errors most commonly made by university students in academic essays. The system embeds comments into your paper and suggests possible changes in grammar and style. Please evaluate each comment carefully to ensure that the suggested change is appropriate for your paper, but remember that your instructor's preferences for style and format prevail. You will also need to review your own citations and references since WritePoint capability in this area is limited. Thank you for using WritePoint. Electronic Medical Record Speech HCR/240 February 4, 2012 Assignment: Electronic Medical Record Speech 2 An Electronic Medical Record is a system that would store the physician's report of the examination, also their surgical procedure, plus the tests the physician's ask for. The Electronic Medical Record is also where they store the x-ray results and also other of the clinical information that is [Wordiness: see if you can remove "that" or "that is"] recorded. There are eight different major features of the Electronic Medical Records and the benefits and [Grammar: A run-on sentence requires a comma before "and" (or other conjunction) linking main clauses] they are: Immediate access to health information and [Grammar: A run-on sentence requires a comma before "and" (or other conjunction) linking main clauses] it is accessible from the workstations in these offices and from a remote site which would be the hospitals at all the same times; Computerized physician order management is where ["is where" or "are where" are awkward phrases; use simply "here"--or reword the sentence to something like "In management", or "With management,"] the physician could enter the medication order and can order tests the for patient plus this can be done at anytime; Clinical decision support and this type of system could provide the access to all the latest of the medical researches; Automated alerts and reminders is where ["is where" or "are where" is awkward wording; use another expression] there systems could provide the medical alerts to help the office staff remember their patients screenings and all other services; Electronic communication and connectivity is the system that would provide a secure and a easy accessible type of communication that is [Wordiness: see if you can remove "that" or "that is"] between the staff and the physicians; Patient support is where ["is where" or "are where" is awkward wording; use another expression] the patient could access their own medical records and could request an appointment electronically; Administrative and reporting is where ["is where" or "are where" is awkward wording; use another expression] the medical practices have to Assignment: Electronic Medical Record Speech 3 comply with the federal and also the state reporting of the requirements; Error reduction would help decrease all the medical errors that can happen due to [Check word usage: This phrase is most accurate in referring to something owed ($5 due) or an arrival time (due at 6:00)--try "because" or "because of"] the illegible chart notes and this is because [Awkward wording-replace "is because" with "is that"--chart notes and this is that] the notes are no longer entered manually. The importance of the practice management is the survival because it is accurate and timely records would be required to help determine if the practice is a profitable. The records are also important because they must meet a financial obligation and also the tax reporting of those requirements
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Arkansas Little Rock - SCIENCE - sci 241
HIPAA and Information Technology Checkpoint1Human DigestionSCI/241 February 3, 2012CheckPoint: Human Digestion2The digestive system is a chain of organs and glands that breaks down the food we eat in order for our bodies to receive the nutrients it
Arkansas Little Rock - SCIENCE - sci 241
HIPAA and Information Technology CheckpointHuman Digestio1SCI/241 February 3, 2012Describe, in 200 to 300 words, the path food follows through the digestive system and how digestion occurs in each of the following parts of the digestive system. Includ
Arkansas Little Rock - SCIENCE - sci 241
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Arkansas Little Rock - SCIENCE - sci 241
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Arkansas Little Rock - SCIENCE - sci 241
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Arkansas Little Rock - SCIENCE - sci 241
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AA 311 Homework 1. Due October 3, 20111. Write a brief essay about why you chose aeronautics and astronautics as your academic career path. (There is no right or wrong answer here.) What is your goal after graduation? 2. Pick three fixed-wing aircraft of
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AA311 Homework 2. Due October 10, 2011Give all your answers in SI units. 1. (Problem 2.1 in [1]) Consider the low-speed flight of the Space Shuttle as it is nearing a landing. If the air pressure and temperature at the nose are p = 1.2 atm and T = 300 K,
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AA311 Homework 2. Due October 10, 2011Give all your answers in SI units. 1. (Problem 2.1 in [1]) Consider the low-speed flight of the Space Shuttle as it is nearing a landing. If the air pressure and temperature at the nose are p = 1.2 atm and T = 300 K,
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AA311 Homework 3. Due October 17, 2011Give all your answers in SI units. Problem 1. Recall that, when developing the equations for the ISA and the notion of "geopotential height," we assumed that g(hG ) g0 . The geopotential height h was then defined suc
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AA311 Homework 3. Due October 17, 2011. Solution.Give all your answers in SI units. Problem 1. Recall that, when developing the equations for the ISA and the notion of "geopotential height," we assumed that g(hG ) g0 . The geopotential height h was then
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AA311 Homework 4. Due November 7, 2011Give all your answers in SI units. Problem 1. An aircraft is flying at a true airspeed of 400 ft/s in standard sea-level conditions. Estimate the pitot pressure (P0 ) based on the incompressible flow form of the Bern
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AA311 Homework 5. Due November 14, 2011Give all your answers in SI units. Problem 1. An aircraft weighs 12, 500 N and has a 20 m2 wing area, an aspect ratio of 6 and efficiency factor e = 0.9. If CD0 = 0.02, (a) Calculate the values of the minimum drag f
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AA311 - Atmospheric Flight Mechanics Autumn 2010 University of Washington Homework 1 SolutionsProblem 1Not applicable.Printed AA311 - Atmospheric Flight Mechanics by Mathematica for StudentsChristopher Lum2hw01_solutions.nbProblem 2Using the equat
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AA311 - Atmospheric Flight Mechanics Autumn 2010 University of Washington Homework 2 SolutionsProblem 1Part a.From the problem statement we know that g0 = 24.9 m s2 R = 4157J kg KT = 150 Kg0 = 24.9; R = 4157; T = 150;Since the atmosphere is assumed
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AA311 - Atmospheric Flight Mechanics Autumn 2010 University of Washington Homework 3 SolutionsProblem 1Part a.From Appendix B, at h = 50 000 ft, the temperature is T = 389.99 RTinfty = 389.99;The free stream speed of sound is a= gRTwhere g = 1.4 R =
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AA311 - Atmospheric Flight Mechanics Autumn 2010 University of Washington Homework 4 SolutionsProblem 1We can find pressure at free stream as using Appendix A with hG = 3000 m p = 7.0121 104 N m2pinfty = 7.0121 104 ;Because the flow is assumed isentro
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AA311 - Atmospheric Flight Mechanics Autumn 2010 University of Washington Homework 5 SolutionsProblem 1Part a.For standard sea level conditions T = 288.16 K r = 1.225 kg m3p = 1.01325 105 N m2Tinfty = 288.16; infty = 1.225; pinfty = 1.01325 105 ;We
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AA311 - Atmospheric Flight Mechanics Autumn 2010 University of Washington Homework 6 SolutionsProblem 1Part a.We can first convert to consistent, metric units F-14 S = 54.5 m2 W = 52 000 lbf .4.44822162 N 1 lbf. = 231 308 N . = 123 661 N i = 1, 2 (th
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AA311 - Atmospheric Flight Mechanics Autumn 2010 University of Washington Homework 7 SolutionsProblem 1We can plot the data. From this we see that the drag polar should be described by CD = CD,0 +CL 2 p e ARNote that we can write this as y = a1 x2 + a
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AA311 - Atmospheric Flight Mechanics Autumn 2010 University of Washington Homework 8 SolutionsProblem 1Part a.Finding the Rate of Climb First, we seek the maximum climb angle possible, qmax . Finding this requires finding where the power available equa
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AA311 - Atmospheric Flight Mechanics Autumn 2010 University of Washington Homework 9 SolutionsProblem 1Part a.We assume that on first approximation, the horsepower generated is proportional to the altitudePaltitude Psl=raltitude rslwhere Paltitude
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AOE 3104 Aircraft Performance Final Exam Solution Problem 1 (5 points): What is a hybrid airship? (A one sentence description is a sufficient answer) The combination of a heavier than air (HTA) vehicle and a lighter than air (LTA) vehicle i.e. the combin
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AOE 3104 Homework #3 SolutionsProblem 1. An aircraft weighs 12, 500 N and has a 20 m2 wing area, an aspect ratio of 6 and efficiency factor e = 0.9. If CD0 = 0.02, (a) Calculate the values of the minimum drag force Dmin and the airspeed for minimum drag
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AOE 3104 Homework #4 SolutionsProblem 1. A sailplane of mass 500 kg has an aspect ratio A = 22 and a wingspan b = 15 m. The drag R parameter values are CD0 = 0.01 and K = 0.015. The glider is released at 3,000 m on a standard day. Estimate the best range
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AOE 3104 Homework #5Assigned: March 22, 2010 Due: March 29, 2010 (Place your homework in the box outside my office by 5 PM.) For Problems 1 through 3,2 CDTO = 0.02 + 0.04CL ,CLmax,TO = 1.5,VTO = 1.2Vstall ,andTO = 0.02.Problem 1. A certain plane we
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Michael Naper2010.04.21AOE 3104Exam #2Problem 1: Given: = 80 = 44,000 = 2,500 = 150 2 = 2.0 Find: a) the minimum and maximum speed at sea level b) the parameters 0 and (assuming a parabolic drag polar). c) the maximum climb rate at sea level d) the a
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AA 311 Lecture 4: Basic Aerodynamics, Measurement of AirspeedReading: [1] Chapters 4.1-4.3 and 4.11. In this lecture we review a couple of fundamental physical principles, and apply them to derive some fundamental equations used in aerodynamics. These pr
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AA 311 Lecture 5: Airfoil Nomenclature; Lift and DragReading: [1] Chapter 5. Consider the wing of an airplane as depicted in Figure 1. The cross-sectional shape obtained as the intersection of the airplane's wing with a vertical plane perpendicular to th
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AA 311 Lecture 12: Aircraft Performance in Straight & Level FlightReading: [1] Chapter 6.1-6.3. Aircraft performance deals with questions like: What is the maximum speed? What is the minimum speed? How fast can it climb to a given altitude? How far can i
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AA 311 Lecture 16: Range and EnduranceReading: [1] Chapter 6.12-6.13. Two important concepts in aircraft performance are range and endurance. Roughly speaking, range of an airplane is the distance it can cover on a tank of fuel, and endurance is the time
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AA311: Atmospheric Flight Mechanics Lecture 16: Range and EnduranceDr. Laszlo TechyUniversity of Washington Department of Aeronautics & AstronauticsNovember 09, 2011Dr. Laszlo TechyAA311: Atmospheric Flight MechanicsRange and EnduranceRange: How fa
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AA 311 Lecture 19: Introduction to Static StabilityTo discuss stability of a steady motion, we must first introduce some terminology to describe the motion. Suppose we fix a reference frame to some point in the aircraft, as shown in Figure 1. We denote b
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AA 311 Lecture 20: Static StabilityTransferring moments. Recall that in the previous lecture we began discussing static longitudinal stability. We obtained requirements on the dimensionless pitch moment coefficient as a function of the angle of attack .
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