How to Measure Navigational Velocity Using the Metric System by Stanley M
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So, What Is Actually the Distance from the Equator to the Pole? – Overview of the Meridian Distance Approximations
the International Journal Volume 7 on Marine Navigation Number 2 http://www.transnav.eu and Safety of Sea Transportation June 2013 DOI: 10.12716/1001.07.02.14 So, What is Actually the Distance from the Equator to the Pole? – Overview of the Meridian Distance Approximations A. Weintrit Gdynia Maritime University, Gdynia, Poland ABSTRACT: In the paper the author presents overview of the meridian distance approximations. He would like to find the answer for the question what is actually the distance from the equator to the pole ‐ the polar distance. In spite of appearances this is not such a simple question. The problem of determining the polar distance is a great opportunity to demonstrate the multitude of possible solutions in common use. At the beginning of the paper the author discusses some approximations and a few exact expressions (infinite sums) to calculate perimeter and quadrant of an ellipse, he presents convenient measurement units of the distance on the surface of the Earth, existing methods for the solution of the great circle and great elliptic sailing, and in the end he analyses and compares geodetic formulas for the meridian arc length. 1 INTRODUCTION navigational receivers and navigational systems (ECDIS and ECS [Weintrit, 2009]) suggest the Unfortunately, from the early days of the necessity of a thorough examination, modification, development of the basic navigational software built verification and unification of the issue of sailing into satellite navigational receivers and later into calculations for navigational systems and receivers. electronic chart systems, it has been noted that for the The problem of determining the distance from the sake of simplicity and a number of other, often equator to the pole is a great opportunity to incomprehensible reasons, this navigational software demonstrate the multitude of possible solutions in is often based on the simple methods of limited common use. -
Calculating Growing Degree Days by Jim Nugent District Horticulturist Michigan State University
Calculating Growing Degree Days By Jim Nugent District Horticulturist Michigan State University Are you calculating degree day accumulations and finding your values don't match the values being reported by MSU or your neighbor's electronic data collection unit? There is a logical reason! Three different methods are used to calculate degree days; i.e., 1) Averaging Method; 2) Baskerville-Emin (BE) Method; and 3) Electronic Real-time Data Collection. All methods attempt to calculate the heat accumulation above a minimum threshold temperature, often referred to the base temperature. Once both the daily maximum and minimum temperatures get above the minimum threshold temperature, (i.e., base temperature of 42degrees, 50degrees or whatever other base temperature of interest) then all methods are fairly comparable. However, differences do occur and these are accentuated in an exceptionally long period of cool spring temperatures, such as we experienced this year. Let me briefly explain: 1. Averaging Method: Easy to calculate Degree Days(DD) = Average daily temp. - Base Temp. = (max. + min.) / 2 - Base temp. If answer is negative, assume 0. Example: Calculate DD Base 50 given 65 degrees max. and 40 degrees min. Avg. = (65 + 40) / 2 = 52.5 degrees DD base 50 = 52.5 - 50 = 2.5 degrees. But look what happens given a maximum of 60 degrees and a minimum of 35 degrees: Avg. = (60 + 35) / 2 = 47.5 DD base 50 = 47.5 - 50 = -2.5 = 0 degrees. The maximum temperature was higher than the base of 50° , but no degree days were accumulated. A grower called about the first of June reporting only about 40% of the DD50 that we have recorded. -
Soaring Weather
Chapter 16 SOARING WEATHER While horse racing may be the "Sport of Kings," of the craft depends on the weather and the skill soaring may be considered the "King of Sports." of the pilot. Forward thrust comes from gliding Soaring bears the relationship to flying that sailing downward relative to the air the same as thrust bears to power boating. Soaring has made notable is developed in a power-off glide by a conven contributions to meteorology. For example, soar tional aircraft. Therefore, to gain or maintain ing pilots have probed thunderstorms and moun altitude, the soaring pilot must rely on upward tain waves with findings that have made flying motion of the air. safer for all pilots. However, soaring is primarily To a sailplane pilot, "lift" means the rate of recreational. climb he can achieve in an up-current, while "sink" A sailplane must have auxiliary power to be denotes his rate of descent in a downdraft or in come airborne such as a winch, a ground tow, or neutral air. "Zero sink" means that upward cur a tow by a powered aircraft. Once the sailcraft is rents are just strong enough to enable him to hold airborne and the tow cable released, performance altitude but not to climb. Sailplanes are highly 171 r efficient machines; a sink rate of a mere 2 feet per second. There is no point in trying to soar until second provides an airspeed of about 40 knots, and weather conditions favor vertical speeds greater a sink rate of 6 feet per second gives an airspeed than the minimum sink rate of the aircraft. -
16.00 Introduction to Aerospace and Design Problem Set #3 AIRCRAFT
16.00 Introduction to Aerospace and Design Problem Set #3 AIRCRAFT PERFORMANCE FLIGHT SIMULATION LAB Note: You may work with one partner while actually flying the flight simulator and collecting data. Your write-up must be done individually. You can do this problem set at home or using one of the simulator computers. There are only a few simulator computers in the lab area, so not leave this problem to the last minute. To save time, please read through this handout completely before coming to the lab to fly the simulator. Objectives At the end of this problem set, you should be able to: • Take off and fly basic maneuvers using the flight simulator, and describe the relationships between the control yoke and the control surface movements on the aircraft. • Describe pitch - airspeed - vertical speed relationships in gliding performance. • Explain the difference between indicated and true airspeed. • Record and plot airspeed and vertical speed data from steady-state flight conditions. • Derive lift and drag coefficients based on empirical aircraft performance data. Discussion In this lab exercise, you will use Microsoft Flight Simulator 2000/2002 to become more familiar with aircraft control and performance. Also, you will use the flight simulator to collect aircraft performance data just as it is done for a real aircraft. From your data you will be able to deduce performance parameters such as the parasite drag coefficient and L/D ratio. Aircraft performance depends on the interplay of several variables: airspeed, power setting from the engine, pitch angle, vertical speed, angle of attack, and flight path angle. -
The Discovery of the Sea
The Discovery of the Sea "This On© YSYY-60U-YR3N The Discovery ofthe Sea J. H. PARRY UNIVERSITY OF CALIFORNIA PRESS Berkeley • Los Angeles • London Copyrighted material University of California Press Berkeley and Los Angeles University of California Press, Ltd. London, England Copyright 1974, 1981 by J. H. Parry All rights reserved First California Edition 1981 Published by arrangement with The Dial Press ISBN 0-520-04236-0 cloth 0-520-04237-9 paper Library of Congress Catalog Card Number 81-51174 Printed in the United States of America 123456789 Copytightad material ^gSS3S38SSSSSSSSSS8SSgS8SSSSSS8SSSSSS©SSSSSSSSSSSSS8SSg CONTENTS PREFACE ix INTROn ilCTION : ONE S F A xi PART J: PRE PARATION I A RELIABLE SHIP 3 U FIND TNG THE WAY AT SEA 24 III THE OCEANS OF THE WORI.n TN ROOKS 42 ]Jl THE TIES OF TRADE 63 V THE STREET CORNER OF EUROPE 80 VI WEST AFRICA AND THE ISI ANDS 95 VII THE WAY TO INDIA 1 17 PART JJ: ACHJF.VKMKNT VIII TECHNICAL PROBL EMS AND SOMITTONS 1 39 IX THE INDIAN OCEAN C R O S S T N C. 164 X THE ATLANTIC C R O S S T N C 1 84 XJ A NEW WORT D? 20C) XII THE PACIFIC CROSSING AND THE WORI.n ENCOMPASSED 234 EPILOC.IJE 261 BIBLIOGRAPHIC AI. NOTE 26.^ INDEX 269 LIST OF ILLUSTRATIONS 1 An Arab bagMa from Oman, from a model in the Science Museum. 9 s World map, engraved, from Ptolemy, Geographic, Rome, 1478. 61 3 World map, woodcut, by Henricus Martellus, c. 1490, from Imularium^ in the British Museum. -
Angles ANGLE Topics • Coterminal Angles • Defintion of an Angle
Angles ANGLE Topics • Coterminal Angles • Defintion of an angle • Decimal degrees to degrees, minutes, seconds by hand using the TI-82 or TI-83 Plus • Degrees, seconds, minutes changed to decimal degree by hand using the TI-82 or TI-83 Plus • Standard position of an angle • Positive and Negative angles ___________________________________________________________________________ Definition: Angle An angle is created when a half-ray (the initial side of the angle) is drawn out of a single point (the vertex of the angle) and the ray is rotated around the point to another location (becoming the terminal side of the angle). An angle is created when a half-ray (initial side of angle) A: vertex point of angle is drawn out of a single point (vertex) AB: Initial side of angle. and the ray is rotated around the point to AC: Terminal side of angle another location (becoming the terminal side of the angle). Hence angle A is created (also called angle BAC) STANDARD POSITION An angle is in "standard position" when the vertex is at the origin and the initial side of the angle is along the positive x-axis. Recall: polynomials in algebra have a standard form (all the terms have to be listed with the term having the highest exponent first). In trigonometry, there is a standard position for angles. In this way, we are all talking about the same thing and are not trying to guess if your math solution and my math solution are the same. Not standard position. Not standard position. This IS standard position. Initial side not along Initial side along negative Initial side IS along the positive x-axis. -
Maps and Charts
Name:______________________________________ Maps and Charts Lab He had bought a large map representing the sea, without the least vestige of land And the crew were much pleased when they found it to be, a map they could all understand - Lewis Carroll, The Hunting of the Snark Map Projections: All maps and charts produce some degree of distortion when transferring the Earth's spherical surface to a flat piece of paper or computer screen. The ways that we deal with this distortion give us various types of map projections. Depending on the type of projection used, there may be distortion of distance, direction, shape and/or area. One type of projection may distort distances but correctly maintain directions, whereas another type may distort shape but maintain correct area. The type of information we need from a map determines which type of projection we might use. Below are two common projections among the many that exist. Can you tell what sort of distortion occurs with each projection? 1 Map Locations The latitude-longitude system is the standard system that we use to locate places on the Earth’s surface. The system uses a grid of intersecting east-west (latitude) and north-south (longitude) lines. Any point on Earth can be identified by the intersection of a line of latitude and a line of longitude. Lines of latitude: • also called “parallels” • equator = 0° latitude • increase N and S of the equator • range 0° to 90°N or 90°S Lines of longitude: • also called “meridians” • Prime Meridian = 0° longitude • increase E and W of the P.M. -
Guide for the Use of the International System of Units (SI)
Guide for the Use of the International System of Units (SI) m kg s cd SI mol K A NIST Special Publication 811 2008 Edition Ambler Thompson and Barry N. Taylor NIST Special Publication 811 2008 Edition Guide for the Use of the International System of Units (SI) Ambler Thompson Technology Services and Barry N. Taylor Physics Laboratory National Institute of Standards and Technology Gaithersburg, MD 20899 (Supersedes NIST Special Publication 811, 1995 Edition, April 1995) March 2008 U.S. Department of Commerce Carlos M. Gutierrez, Secretary National Institute of Standards and Technology James M. Turner, Acting Director National Institute of Standards and Technology Special Publication 811, 2008 Edition (Supersedes NIST Special Publication 811, April 1995 Edition) Natl. Inst. Stand. Technol. Spec. Publ. 811, 2008 Ed., 85 pages (March 2008; 2nd printing November 2008) CODEN: NSPUE3 Note on 2nd printing: This 2nd printing dated November 2008 of NIST SP811 corrects a number of minor typographical errors present in the 1st printing dated March 2008. Guide for the Use of the International System of Units (SI) Preface The International System of Units, universally abbreviated SI (from the French Le Système International d’Unités), is the modern metric system of measurement. Long the dominant measurement system used in science, the SI is becoming the dominant measurement system used in international commerce. The Omnibus Trade and Competitiveness Act of August 1988 [Public Law (PL) 100-418] changed the name of the National Bureau of Standards (NBS) to the National Institute of Standards and Technology (NIST) and gave to NIST the added task of helping U.S. -
Applications of Geometry and Trigonometry
P1: FXS/ABE P2: FXS 9780521740517c14.xml CUAU031-EVANS September 6, 2008 13:36 CHAPTER 14 MODULE 2 Applications of geometry and trigonometry How do we apply trigonometric techniques to problems involving angles of depression and elevation? How do we apply trigonometric techniques to problems involving bearings? How do we apply trigonometric techniques to three-dimensional problems? How do we draw and interpret contour maps? How do we draw and interpret scale drawings? 14.1 Angles of elevation and depression, bearings, and triangulation Angles of elevation and depression The angle of elevation is the angle The angle of depression is the angle between the horizontal and a between the horizontal and a direction below direction above the horizontal. the horizontal. eye level line of sight angle of depression line of sight eye level cliff angle of elevation SAMPLEboat Cambridge University Press • Uncorrected Sample pages • 978-0-521-61328-6 • 2008 © Jones, Evans, Lipson TI-Nspire & Casio ClassPad material in collaboration with Brown410 and McMenamin P1: FXS/ABE P2: FXS 9780521740517c14.xml CUAU031-EVANS September 6, 2008 13:36 Chapter 14 — Applications of geometry and trigonometry 411 Bearings The three-figure bearing (or compass bearing) is the direction measured clockwise from north. The bearing of A from O is 030◦. The bearing of C from O is 210◦. The bearing of B from O is 120◦. The bearing of D from O is 330◦. N D N A 30° 330° E 120° E W O 210° W O B C S S Example 1 Angle of depression The pilot of a helicopter flying at 400 m observes a small boat at an angle of depression of 1.2◦. -
Tail Strikes: Prevention Regardless of Airplane Model, Tail Strikes Can Have a Number of Causes, Including Gusty Winds and Strong Crosswinds
Tail Strikes: Prevention Regardless of airplane model, tail strikes can have a number of causes, including gusty winds and strong crosswinds. But environmental factors such as these can often be overcome by a well-trained and knowledgeable flight crew following prescribed procedures. Boeing conducts extensive research into the causes of tail strikes and continually looks for design solutions to prevent them, such as an improved elevator feel system. Enhanced preventive measures, such as the tail strike protection feature in some by Capt. Dave Carbaugh, Chief Pilot, Boeing 777 models, further reduce the probability of incidents. Flight Operations Safety Tail strikes can cause significant damage and cost taiL strikes: an overview a constant feel elevator pressure, which has operators millions of dollars in repairs and lost reduced the potential of varied feel pressure revenue. In the most extreme scenario, a tail strike A tail strike occurs when the tail of an airplane on the yoke contributing to a tail strike. The can cause pressure bulkhead failure, which can strikes the ground during takeoff or landing. 747-400 has a lower rate of tail strikes than ultimately lead to structural failure; however, long Although many tail strikes occur on takeoff, most the 747-100/-200/-300. shallow scratches that are not repaired correctly occur on landing. Tail strikes are often due to In addition, some 777 models incorporate a tail can also result in increased risks. Yet tail strikes can human error. strike protection system that uses a combination be prevented when flight crews understand their Tail strikes can cause significant damage to of software and hardware to protect the airplane. -
1. What Is the Radian Measure of an Angle Whose Degree Measure Is 72◦ 180◦ 72◦ = Πradians Xradians Solving for X 72Π X = Radians 180 2Π X = Radians 5 Answer: B
1. What is the radian measure of an angle whose degree measure is 72◦ 180◦ 72◦ = πradians xradians Solving for x 72π x = radians 180 2π x = radians 5 Answer: B 2. What is the length of AC? Using Pythagorean Theorem: 162 + b2 = 202 256 + b2 = 400 b2 = 144 b = 12 Answer: E 3. one solution to z2 + 64 = 0 is z2 + 64 = 0 z2 = −64 p p z2 = −64 Since there is a negative under the radical, we get imaginary roots. Thus z = −8i or z = +8i Answer: A 4. Simplifying: p 36x10y12 − 36y12 = p36y12 (x10 − 1) p = 36y12p(x10 − 1) p = 6y6 x10 − 1 Answer: C 1 5. Simplifying: 1 1 1 1 1 −3 9 6 3 −3 9 6 27a b c = 27 3 a 3 b 3 c 3 = 3a−1b3c2 3b3c2 = a Answer: C 6. Solving for x: p 8 + x + 14 = 12 p x + 14 = 12 − 8 p x + 14 = 4 p 2 x + 14 = 42 x + 14 = 16 x = 16 − 14 x = 2 Answer: C 7. Simplify x2 − 9 (x + 1)2 2x − 6 × ÷ x2 − 1 (2x + 3)(x + 3) 1 − x Rewrite as a multiplication. x2 − 9 (x + 1)2 1 − x × x2 − 1 (2x + 3)(x + 3) 2x − 6 Simplify each polynomial (x − 3)(x + 3) (x + 1)(x + 1) 1 − x × (x − 1)(x + 1) (2x + 3)(x + 3) 2(x − 3) Canceling like terms (x + 1) − 2(2x + 3) Answer: C 2 8. Simplifying: 1 11 x−5 11 + 2 2 + 2 x−5 (x−5) = (x−5) (x−5) x + 1 x + 1 x−5+11 2 = (x−5) x + 1 x+6 2 = (x−5) x + 1 x + 6 = (x − 5)2(x + 1) Answer: B 9. -
The Future of the Knot As a Unit of Speed
FORUM The Future of the Knot as a Unit of Speed Oliver Stewart FEW will deny the merits of the knot as a unit of speed. It does in one syllable what all other units of speed take three or more to do. It is accepted and used by a great many countries, including those like France which show a general pre- ference for the metric system. Aviation has taken to it as well as shipping. It is not therefore surprising that the full acceptance of the Systeme International d'Unitis (or S.I.) is meeting with some opposition when it offers to supplant the knot. At present the situation is that the knot is to continue for a 'limited time' as a speed unit for use in aviation and shipping. Just how limited the time will be has not been revealed, but the member countries of the European Economic Com- munity have set i January 1978 as the date after which 'only a prescribed system of metric units may be used'. Strictly interpreted the S.I. admits one and only one speed unit, the metre per second; if the minute or the hour were to be intro- duced in place of the second, decimalization would break down. This would mean that the familiar kilometre per hour would be inadmissible as a substitute for the knot, although the present trend is in that direction. Both the metre and the second are now denned in terms of atomic radiation with a precision far ahead of anything previously known and give the measurer the highest attainable accuracy.