Glider Handbook, Chapter 10: Soaring Techniques
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Chapter 2 Aviation Weather Hazards
NUNAVUT-E 11/12/05 10:34 PM Page 9 LAKP-Nunavut and the Arctic 9 Chapter 2 Aviation Weather Hazards Introduction Throughout its history, aviation has had an intimate relationship with the weather. Time has brought improvements - better aircraft, improved air navigation systems and a systemized program of pilot training. Despite this, weather continues to exact its toll. In the aviation world, ‘weather’ tends to be used to mean not only “what’s happen- ing now?” but also “what’s going to happen during my flight?”. Based on the answer received, the pilot will opt to continue or cancel his flight. In this section we will examine some specific weather elements and how they affect flight. Icing One of simplest assumptions made about clouds is that cloud droplets are in a liquid form at temperatures warmer than 0°C and that they freeze into ice crystals within a few degrees below zero. In reality, however, 0°C marks the temperature below which water droplets become supercooled and are capable of freezing. While some of the droplets actually do freeze spontaneously just below 0°C, others persist in the liquid state at much lower temperatures. Aircraft icing occurs when supercooled water droplets strike an aircraft whose temperature is colder than 0°C. The effects icing can have on an aircraft can be quite serious and include: Lift Decreases Drag Stall Speed Increases Increases Weight Increases Fig. 2-1 - Effects of icing NUNAVUT-E 11/12/05 10:34 PM Page 10 10 CHAPTER TWO • disruption of the smooth laminar flow over the wings causing a decrease in lift and an increase in the stall speed. -
Understanding the Value of Arts & Culture | the AHRC Cultural Value
Understanding the value of arts & culture The AHRC Cultural Value Project Geoffrey Crossick & Patrycja Kaszynska 2 Understanding the value of arts & culture The AHRC Cultural Value Project Geoffrey Crossick & Patrycja Kaszynska THE AHRC CULTURAL VALUE PROJECT CONTENTS Foreword 3 4. The engaged citizen: civic agency 58 & civic engagement Executive summary 6 Preconditions for political engagement 59 Civic space and civic engagement: three case studies 61 Part 1 Introduction Creative challenge: cultural industries, digging 63 and climate change 1. Rethinking the terms of the cultural 12 Culture, conflict and post-conflict: 66 value debate a double-edged sword? The Cultural Value Project 12 Culture and art: a brief intellectual history 14 5. Communities, Regeneration and Space 71 Cultural policy and the many lives of cultural value 16 Place, identity and public art 71 Beyond dichotomies: the view from 19 Urban regeneration 74 Cultural Value Project awards Creative places, creative quarters 77 Prioritising experience and methodological diversity 21 Community arts 81 Coda: arts, culture and rural communities 83 2. Cross-cutting themes 25 Modes of cultural engagement 25 6. Economy: impact, innovation and ecology 86 Arts and culture in an unequal society 29 The economic benefits of what? 87 Digital transformations 34 Ways of counting 89 Wellbeing and capabilities 37 Agglomeration and attractiveness 91 The innovation economy 92 Part 2 Components of Cultural Value Ecologies of culture 95 3. The reflective individual 42 7. Health, ageing and wellbeing 100 Cultural engagement and the self 43 Therapeutic, clinical and environmental 101 Case study: arts, culture and the criminal 47 interventions justice system Community-based arts and health 104 Cultural engagement and the other 49 Longer-term health benefits and subjective 106 Case study: professional and informal carers 51 wellbeing Culture and international influence 54 Ageing and dementia 108 Two cultures? 110 8. -
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. -
Orographic Rainfall
October f.967 R. P. Sarker 67 3 SOME MODIFICATONS IN A DYNAMICAL MODEL OF OROGRAPHIC RAINFALL R. P. SARKER lnstitufe of Tropical Meteorology, Poona, India ABSTRACT A dynamical model presented earlier by the author for the orographic rainfall over the Western Ghats and based on analytical solutions is modified here in three respects with the aid of numerical methods. Like the earlier approxi- mate model, the modified model also assumes a saturated atmosphere with pseudo-adiabatic lapse rate and is based on linearized equations. The rainfall, as coniputed from the modified model, is in good agreement, both in intensity and in distribution, with the observed rainfall on the windward side of the mountain. Also the modified model suggests that rainfall due to orography may extend out to about 40 km. or so on the lee side from the crest of the mountain and thus explains at least a part of the lee-side rainfall. 1. INTRODUCTION tion for vertical velocity and streamline displacement from the linearized equations with the real distribution of In a previous paper the author [6] proposed a dynamical f (z) as far as possible, subject to the assumption that (a) model of orographic rainfall with particular reference to the ground profile is still a smoothed one, and that (b) the the Western Ghats of India and showed that the model atmosphere is saturated in which both the process and the explains quite satisfactorily the rainfall distribution from environment have the pseudo-adiabatic lapse rate. the coast inland along the orography on the windward side. However, the rainfall distribution as computed from We shall make another important modification. -
Stratospheric Gravity Wave Fluxes and Scales During DEEPWAVE
JULY 2016 S M I T H E T A L . 2851 Stratospheric Gravity Wave Fluxes and Scales during DEEPWAVE 1 RONALD B. SMITH,* ALISON D. NUGENT,* CHRISTOPHER G. KRUSE,* DAVID C. FRITTS, # @ & JAMES D. DOYLE, STEVEN D. ECKERMANN, MICHAEL J. TAYLOR, ANDREAS DÖRNBRACK,** 11 ## ## ## ## M. UDDSTROM, WILLIAM COOPER, PAVEL ROMASHKIN, JORGEN JENSEN, AND STUART BEATON * Department of Geology and Geophysics, Yale University, New Haven, Connecticut 1 GATS, Boulder, Colorado # Naval Research Laboratory, Monterey, California @ Naval Research Laboratory, Washington, D.C. & Utah State University, Logan, Utah ** German Aerospace Center (DLR), Oberpfaffenhofen, Germany 11 National Institute of Water and Atmospheric Research, Kilbirnie, Wellington, New Zealand ## National Center for Atmospheric Research, Boulder, Colorado (Manuscript received 27 October 2015, in final form 25 February 2016) ABSTRACT During the Deep Propagating Gravity Wave Experiment (DEEPWAVE) project in June and July 2014, the Gulfstream V research aircraft flew 97 legs over the Southern Alps of New Zealand and 150 legs over the Tasman Sea and Southern Ocean, mostly in the low stratosphere at 12.1-km altitude. Improved instrument calibration, redundant sensors, longer flight legs, energy flux estimation, and scale analysis revealed several new gravity wave properties. Over the sea, flight-level wave fluxes mostly fell below the detection threshold. Over terrain, disturbances had characteristic mountain wave attributes of positive vertical energy flux (EFz), negative zonal momentum flux, and upwind horizontal energy flux. In some cases, the fluxes changed rapidly within an 8-h flight, even though environ- mental conditions were nearly unchanged. The largest observed zonal momentum and vertical energy fluxes were 22 MFx 52550 mPa and EFz 5 22 W m , respectively. -
Madison Community Foundation 2020 Annual Report
Annual Report 2020 On the Cover The Downtown Street Art and Mural Project As the nation struggled to contain the coronavirus pandemic, it was further rocked by the death of George Floyd on May 25 while in the custody of the Minneapolis police. Floyd’s death set off protests across the nation, and around the world. In Madison, peaceful daytime protests were followed by looting in the evenings, which forced many businesses to shutter their storefronts with plywood. The Madison Arts Commission, funded in part by a Community Impact grant from Madison Community Foundation (MCF), responded to the bleak sight of State Street by creating the Downtown Street Art and Mural Project, which engaged dozens of local artists to use these spaces as an opportunity for expression and civic engagement. More than 100 murals, including the one on our cover, were painted in and around State Street, creating a vibrant visual dialogue addressing racism, memorializing lost lives and inspiring love. Artists participated in panel discussions and were highlighted in local and national media. “Let’s Talk About It: The Art, The Artists and the Racial Justice Movement on Madison’s State Street,” a book focused on the project, was produced by (and is available through) the American Family Insurance Institute for Corporate and Social Impact. In addition, several of the murals will become part of the permanent collection of the Wisconsin Historical Museum. MCF’s long-standing vision — that greater Madison will be a vibrant and generous place where all people thrive — is impossible to achieve without ending racism. We remain committed to this journey. -
Hang Glider: Range Maximization the Problem Is to Compute the flight Inputs to a Hang Glider So As to Provide a Maximum Range flight
Hang Glider: Range Maximization The problem is to compute the flight inputs to a hang glider so as to provide a maximum range flight. This problem first appears in [1]. The hang glider has weight W (glider plus pilot), a lift force L acting perpendicular to its velocity vr relative to the air, and a drag force D acting in a direction opposite to vr. Denote by x the horizontal position of the glider, by vx the horizontal component of the absolute velocity, by y the vertical position, and by vy the vertical component of absolute velocity. The airmass is not static: there is a thermal just 250 meters ahead. The profile of the thermal is given by the following upward wind velocity: 2 2 − x −2.5 x u (x) = u e ( R ) 1 − − 2.5 . a m R We take R = 100 m and um = 2.5 m/s. Note, MKS units are used through- out. The upwind profile is shown in Figure 1. Letting η denote the angle between vr and the horizontal plane, we have the following equations of motion: 1 x˙ = vx, v˙x = m (−L sin η − D cos η), 1 y˙ = vy, v˙y = m (L cos η − D sin η − W ) with q vy − ua(x) 2 2 η = arctan , vr = vx + (vy − ua(x)) , vx 1 1 L = c ρSv2,D = c (c )ρSv2,W = mg. 2 L r 2 D L r The glider is controlled by the lift coefficient cL. The drag coefficient is assumed to depend on the lift coefficient as 2 cD(cL) = c0 + kcL where c0 = 0.034 and k = 0.069662. -
Module-7 Lecture-29 Flight Experiment
Module-7 Lecture-29 Flight Experiment: Instruments used in flight experiment, pre and post flight measurement of aircraft c.g. Module Agenda • Instruments used in flight experiments. • Pre and post flight measurement of center of gravity. • Experimental procedure for the following experiments. (a) Cruise Performance: Estimation of profile Drag coefficient (CDo ) and Os- walds efficiency (e) of an aircraft from experimental data obtained during steady and level flight. (b) Climb Performance: Estimation of Rate of Climb RC and Absolute and Service Ceiling from experimental data obtained during steady climb flight (c) Estimation of stick free and fixed neutral and maneuvering point using flight data. (d) Static lateral-directional stability tests. (e) Phugoid demonstration (f) Dutch roll demonstration 1 Instruments used for experiments1 1. Airspeed Indicator: The airspeed indicator shows the aircraft's speed (usually in knots ) relative to the surrounding air. It works by measuring the ram-air pressure in the aircraft's Pitot tube. The indicated airspeed must be corrected for air density (which varies with altitude, temperature and humidity) in order to obtain the true airspeed, and for wind conditions in order to obtain the speed over the ground. 2. Attitude Indicator: The attitude indicator (also known as an artificial horizon) shows the aircraft's relation to the horizon. From this the pilot can tell whether the wings are level and if the aircraft nose is pointing above or below the horizon. This is a primary instrument for instrument flight and is also useful in conditions of poor visibility. Pilots are trained to use other instruments in combination should this instrument or its power fail. -
2 the Assyrian Empire, the Conquest of Israel, and the Colonization of Judah 37 I
ISRAEL AND EMPIRE ii ISRAEL AND EMPIRE A Postcolonial History of Israel and Early Judaism Leo G. Perdue and Warren Carter Edited by Coleman A. Baker LONDON • NEW DELHI • NEW YORK • SYDNEY 1 Bloomsbury T&T Clark An imprint of Bloomsbury Publishing Plc Imprint previously known as T&T Clark 50 Bedford Square 1385 Broadway London New York WC1B 3DP NY 10018 UK USA www.bloomsbury.com Bloomsbury, T&T Clark and the Diana logo are trademarks of Bloomsbury Publishing Plc First published 2015 © Leo G. Perdue, Warren Carter and Coleman A. Baker, 2015 All rights reserved. No part of this publication may be reproduced or transmitted in any form or by any means, electronic or mechanical, including photocopying, recording, or any information storage or retrieval system, without prior permission in writing from the publishers. Leo G. Perdue, Warren Carter and Coleman A. Baker have asserted their rights under the Copyright, Designs and Patents Act, 1988, to be identified as Authors of this work. No responsibility for loss caused to any individual or organization acting on or refraining from action as a result of the material in this publication can be accepted by Bloomsbury or the authors. British Library Cataloguing-in-Publication Data A catalogue record for this book is available from the British Library. ISBN: HB: 978-0-56705-409-8 PB: 978-0-56724-328-7 ePDF: 978-0-56728-051-0 Library of Congress Cataloging-in-Publication Data A catalogue record for this book is available from the British Library. Typeset by Forthcoming Publications (www.forthpub.com) 1 Contents Abbreviations vii Preface ix Introduction: Empires, Colonies, and Postcolonial Interpretation 1 I. -
THE INFRARED CLOUD IMAGER by Brentha Thurairajah a Thesis Submitted in Partial Fulfi
THERMAL INFRARED IMAGING OF THE ATMOSPHERE: THE INFRARED CLOUD IMAGER by Brentha Thurairajah A thesis submitted in partial fulfillment of the requirements of the degree of Master of Science in Electrical Engineering MONTANA STATE UNIVERSITY Bozeman, Montana April 2004 © COPYRIGHT by Brentha Thurairajah 2004 All Rights Reserved ii APPROVAL of a thesis submitted by Brentha Thurairajah This thesis has been read by each member of the thesis committee and has been found to be satisfactory regarding content, English usage, format, citations, bibliographic style, and consistency, and is ready for submission to the college of graduate studies. Dr. Joseph A. Shaw, Chair of Committee Approved for the Department of Electrical and Computer Engineering Dr. James N. Peterson, Department Head Approved for the College of Graduate Studies Dr. Bruce R. McLeod, Graduate Dean iii STATEMENT OF PERMISSION TO USE In presenting this thesis in partial fulfillment of the requirements for a master’s degree at Montana State University, I agree that the Library shall make it available to borrowers under the rules of the Library. If I have indicated my intention to copyright this thesis by including a copyright notice page, copying is allowable only for scholarly purposes, consistent with “fair use” as prescribed in the U.S Copyright Law. Requests for permission for extended quotation from or reproduction of this thesis in whole or in parts may be granted only by the copyright holder. Brentha Thurairajah April 2nd, 2004 iv ACKNOWLEDGEMENT I would like to thank my advisor Dr. Joseph Shaw for always being there, for guiding me with patience throughout the project, for helping me with my course and research work through all these three years, and for providing helpful comments and constructive criticism that helped me complete this document. -
Revised for Release Feb. 19, 2016 Media Contact: Laura Carpenter
625 C Street, Anchorage AK 99501 Revised for release Feb. 19, 2016 Media Contact: Laura Carpenter, (907) 929-9227, [email protected] SCHEDULE OF PROGRAMS AND EXHIBITIONS MARCH/APRIL 2016 *EDITORS PLEASE NOTE: This release replaces previous schedules. Download related media images at www.anchoragemuseum.org/media. Information provided below is subject to change. To confirm details and dates, call the Marketing and Public Relations Department at (907) 929-9227. News page 1 March Events page 2 April Events page 5 Planetarium page 6 Classes and Workshops page 8 Upcoming Exhibitions page 9 Current Exhibitions page 10 Partner Programs page 11 Visitor Information page 12 NEWS Artists invited to apply for exhibitions at the Anchorage Museum The Anchorage Museum is accepting submissions until March 10 for project proposals for solo and group exhibitions. The Anchorage Museum’s Patricia B. Wolf Solo Exhibition Series supports the work and development of Alaska artists, highlighting new bodies of work by individual artists. Alaska artists are invited to submit applications to a selection committee comprised of museum staff and art professionals. These solo art exhibitions will be scheduled starting in 2017. The Anchorage Museum is currently accepting proposals from Alaska residents and all tribally enrolled Alaska Natives. Works in all media will be considered. The Anchorage Museum is also accepting curatorial and group proposals featuring more than one artist. These proposals will not be part of the Patricia B. Wolf exhibition series but will be brought before the museum’s Exhibition Review Committee for consideration. Applicants for group and curatorial proposals do not need to be from Alaska, but successful proposals will support the museum’s mission to connect people, expand perspectives and encourage global dialogue about the North and its distinct environment. -
How to Make My Air Glide S Work Properly
How to make my Air Glide S work properly Originally written by Horst Rupp. Many thanks to Richard Frawley who edited and retranslated this article into proper English. 2014/11/21. The basic prerequisite for the Air Glide S, in particular the AHRS part, to work properly so that the extraneous ‘noise’ (gusts, wind shifts, perturbations etc) can be removed is to ensure that it is set up correctly. The instrument is very sensitive and the installation needs to be done in a way that ensures that only the correct inputs are being sensed. Most legacy instrument installations take all pressures from probes at the rudder fin. And most unfortunately, many of them use the total energy (TE) pressure from the fin to feed in parallel a mass-measurement variometer with a capacity flask (in Germany mostly a Winter) and a pressure sensor probe variometer such as the Air Glide S (no capacity flask). There are many publications indicating the deterioration (mostly damping) of the pressure sensor probe measurements by the stream of air mass in and out of the capacity flask. So, it is obviously a somewhat bad idea to do that to your Air Glide S. This interference with a mass measuring instruments is certainly not compliant with the above mentioned basic prerequisite. Fortunately, the Air Glide S can be compensated by total pressure (called electronic compensation as opposed to TE compensation). This is a new feature of the Air Glide S arriving with V 1.1. Total pressure and TE pressure carry more or less (depends on quality of probe) the same information - but for the sign : Total pressure is static pressure PLUS pitot pressure, TE pressure is static pressure MINUS pitot pressure (probe compensation factor (~)-1).