The Art of Soaring Flight
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IGC Plenary 2005
Agenda of the Annual Meeting of the FAI Gliding Commission To be held in Lausanne, Switzerland on 5th and 6th March 2010 Agenda for the IGC Plenary 2010 Day 1, Friday 5th March 2010 Session: Opening and Reports (Friday 09.15 – 10.45) 1. Opening (Bob Henderson) 1.1 Roll Call (Stéphane Desprez/Peter Eriksen) 1.2 Administrative matters (Peter Eriksen) 1.3 Declaration of Conflicts of Interest 2. Minutes of previous meeting, Lausanne, 6th-7th March 2009 (Peter Eriksen) 3. IGC President’s report (Bob Henderson) 4. FAI Matters (Mr.Stéphane Desprez) 4.1 Update by the Secretary General 5. Finance (Dick Bradley) 5.1 2009 Financial report 5.2 Financial statement and budget 6. Reports not requiring voting 6.1 OSTIV report (Loek Boermans) Please note that reports under Agenda items 6.2, 6.3 and 6.4 are made available on the IGC web-site, and will not necessarily be presented. The Committees and Specialists will be available for questions. 6.2 Standing Committees 6.2.1 Communications and PR Report (Bob Henderson) 6.2.2 Championship Management Committee Report (Eric Mozer) 6.2.3 Sporting Code Committee Report (Ross Macintyre) 6.2.4 Air Traffic, Navigation, Display Systems (ANDS) Report (Bernald Smith) 6.2.5 GNSS Flight Recorder Approval Committee (GFAC) Report (Ian Strachan) 6.2.6 FAI Commission on Airspace and Navigation Systems (CANS) Report (Ian Strachan) Session: Reports from Specialists and Competitions (Friday 11.15 – 12.45) 6.3 Working Groups 6.3.1 Country Development Report (Alexander Georgas) 6.3.2 Grand Prix Action Plan (Bob Henderson) 6.3.3 History Committee (Tor Johannessen) 6.3.4 Scoring Working Group (Visa-Matti Leinikki) 6.4 IGC Specialists 6.4.1 CASI Report (Air Sports Commissions) (Tor Johannessen) 6.4.2 EGU/EASA Report (Patrick Pauwels) 6.4.3 Environmental Commission Report (Bernald Smith) 6.4.4 Membership (John Roake) 6.4.5 On-Line Contest Report (Axel Reich) 6.4.6 Simulated Gliding Report (Roland Stuck) 6.4.7 Trophy Management Report (Marina Vigorita) 6.4.8 Web Management Report (Peter Ryder) 7. -
Minimoa SN4 April 2019
Magazine for Pilots & Fans of Schempp-Hirth Sailplanes - April 2019 / No.4 Discus-2c “supercharged”: The FES A New Game Is on for a Sailplane Adventures Around the World From Denmark and Canada to the South Hemisphere Formula 1.0: Fun’n’Dust in Australia Old Plastic Tins Get Some Fun with GP Concept Editorial Ralf & Tilo Holighaus / [email protected] 02 Minimoa No. 4, Apr. 2019 > Fly Denmark! 12 > Formula 1.0: Australia 16 CONTRIBUTORS. Jorgen Thomsen, Makoto Ichikawa, Chester Fitchett, Andrew Peng Du, Morten Bennick, Vladimir Fedorov, Nick Gilbert, Adam Lanson, Tilo Holighaus, Ralf Ho - lighaus, Benjamin Neglais Editor: Ralf Holighaus [email protected] Design: Benjamin Neglais, Ralf Holighaus Pictures: Francois Jeremiasse, Benjamin Neglais, Chris Wilson, Morten Bennick, Andrew Peng Du, Makoto Ichikawa, f1gp.com.au, Chester Fitchett > Discus-2c “supercharged”: The FES 04 Editorial Solar Power 2018 was probably one of the best ever years for glid - On the same basis, gliders of all vendors together cir - ing in Europe, with record weather conditions far beyond cled the globe in average 3.75 times every day - and this average. Flights adding up to an amazing 54 Million km figure only covers the flights that were actually uploaded have been scored in the OLC and we are very proud that to the OLC! These figures should help each of you to Schempp-Hirth gliders from Cirrus to Ventus-3 have con - demonstrate to the World that we are one of the most tributed 21 Million km in more than 58,000 flights, rep - environment-friendly sports, having relied on using solar resenting almost 40% of all uploaded kilometers. -
Vistara Soars Toward Expansion New Flight-Planning Technology Enhances Safety, Cuts Costs
MOBILITY ENGINEERINGTM AUTOMOTIVE, AEROSPACE, OFF-HIGHWAY A quarterly publication of and Vistara soars toward expansion New flight-planning technology enhances safety, cuts costs Base-engine value engineering Deriving optimum efficiency, performance Autos & The Internet of Things How the IoT is disrupting the auto industry Software’s expanding role Escalating software volumes shifting design, systems integration Volume 3, Issue 2 June 2016 ME Molex Ad 0616.qxp_Mobility FP 4/28/16 5:00 PM Page 1 Support Tomorrow’s Speeds with Proven Connectivity Simply Solved In Automotive, consumer demand is changing even faster than technology. When you collaborate with Molex, we can develop a complete solution that will support tomorrow’s data speeds, backed by proven performance. Together, we can simplify your design and manufacturing processes — while minimizing space and maximizing connectivity throughout the vehicle. www.molex.com/a/connectedvehicle/in CONTENTS Features 40 Base-engine value engineering 49 Agility training for cars for higher fuel efficiency and AUTOMOTIVE CHASSIS enhanced performance Chassis component suppliers refine vehicle dynamics at AUTOMOTIVE POWERTRAIN the high end and entry level with four-wheel steering and adaptive damping. Continuous improvement in existing engines can be efficiently achieved with a value engineering approach. The integration of product development with value 52 Evaluating thermal design of engineering ensures the achievement of specified targets construction vehicles in a systematic manner and within a defined timeframe. OFF-HIGHWAY SIMULATION CFD simulation is used to evaluate two critical areas that 43 Integrated system engineering address challenging thermal issues: electronic control units for valvetrain design and and hot-air recirculation. development of a high-speed diesel engine AUTOMOTIVE POWERTRAIN The lead time for engine development has reduced significantly with the advent of advanced simulation Cover techniques. -
IN THIS ISSUE PAGE 2 Badges President's Note from the Editor
February, 2014 THE OFFICIAL PUBLICATION OF THE WOMEN SOARING PILOTS ASSOC. www.womensoaring.org IN THIS ISSUE PAGE 2 Badges President’s Note From the Editor PAGE 3 2014 Raffle Announcement Canada Licensing PAGE 5 www.womensoaring.org Berblinger Prize 2013 PROMOTING WOMEN IN SOARING AT EVERY SKILL LEVEL PAGE 6-7 News from around the World OVER $50,000 IN SCHOLARSHIPS GIVEN TO WOMEN PILOTS SINCE ITS INCEPTION PAGE 8 A Little Rositten Gliding ANNUAL WSPA SEMINARS IN THE BEST SOARING SITES AROUND THE WORLD History PAGE 9 News from Former Members Welcome New Members Famous Women Pilots: Hana Zejdova PAGE 10 WSPA History Project PAGE 11 This and That page 2 February 2014 THE WOMEN SOARING PILOTS Badges ASSOCIATION (WSPA) WAS FOUNDED (reported through January 2014) A Badge IN 1986 AND IS AFFILIATED WITH THE Elizabeth Bell, CT SOARING SOCIETY OF AMERICA Gold Altitude Sylvia Blanco, OK Marianne Guerin, NV Melanie Marcols, NJ THE 2013/14 BOARD Julie Butler, CA Bronze Badge Christina Atkins, PA Deonna Neil, CO From the Editor Neita Montague (West) President C Badge I hope everybody had a good 7840 Tamra Dr. Melanie Marcols, NJ Ed note: By the time Hangar Holiday Season and a good transi- Reno, NV 89506 Julie Butler, CA Soaring was ready to go to the tion into the New Year with it a printer I had not received the slew of resolutions including some Maja Djurisic (West) B Badge February SOARING to include soaring related ones. Did you Vice President the February listings in this resolve to solo in the New Year; to Melanie Marcols, NJ issue. -
Flight and Operations Manual for the Sailplane Model a S W 2 0
ALEXANDER SCHLEICHER SEGELFLUGZEUBAU D - 6416 Poppenhausen / Wasserkuppe Flight and Operations Manual for the Sailplane Model A S W 2 0 =========== July, 1977 Edition This manual is always to be carried on board ! It belongs to the sailplane A S W 2 0 Serial No. 20058 Registration No. BGA 2565 Owner : ........................... ........................... ........................... Manufacturer : Alexander Schleicher Segelflugzeugbau D-6416 Poppenhausen This manual is the translation of the German original which is approved by the Federal Office of Civil Aeronautics of the Federal Republic of Germany ( LBA ). The translation has been done by best knowledge and judgement. In any case the original text in German language is authoritative. 1 A S W 20 -Flight Manual Contents Title page Page 1 Contents Page 2+3 Amendments Page 4 1 Flight Manual 1.1. Preface Page 5 Operating Handles, Placards and 1.2. Page 12 Nomenclatures 1.3. Operation Values and Limitations Page 16 1.4. Weight and Balance Information Page 19 1.5. Minimum Equipment Page 21 1.6. Emergency Procedures Page 22 1.7. In Flight Information Page 23 Empty Weight Centre of Gravity 1.8. Page 30 Limits Centre of Gravity at the Last 1.9. Page 31 Weighing 2 Operations Manual 2.1. Rigging Page 32 2.2. Checking Page 34 2.3. Derigging Page 34 2.4. Road Transport Page 34 2.5. Upkeep and Maintenance Page 35 2.6. Overhauls Page 38 2.7. Repairs Page 38 2.8. Notes for the Inspection Page 38 2 A S W 20 -Flight Manual 3. Appendix 3.1. Three-View-Drawing Page 41 3.2. -
United States Patent (19) 11) Patent Number: 4,691,879 Greene 45) Date of Patent: Sep
United States Patent (19) 11) Patent Number: 4,691,879 Greene 45) Date of Patent: Sep. 8, 1987 54 JET AIRPLANE gravity. Full control of the airplane is possible under 76 Inventor: Vibert F. Greene, 19400 Sorenson high maneuverability conditions, extremely high accel Ave., Cupertino, Calif. 95014 erations and at large angles of attack. The delta nose wing creates swirling vortices that contribute substan 21 Appl. No.: 875,024 tially to the lift of the nose section. The winglet, an 22). Filed: Jun. 16, 1986 extension of the delta nose wing, allows the turbulent wake from the leading edge of the delta nose wing to 51 Int. Cl." .............................................. B64C39/08 flow over its upper surface to create additional lift while 52 U.S.C. .................................... 244/45 R; 24.4/13; the midspan wing causes the turbulent flow over its 244/45 A; 244/15 upper surface to form a turbulent wake at its leading 58 Field of Search .................. 244/45 R, 45 A, 4 R, edge. The V-tail delta wing with a V-shaped underside 244/15, 13 and blunt leading edge gives additional lift and control (56) References Cited to the airplane. A flow regulator helps to direct and U.S. PATENT DOCUMENTS control the flow field to the underside of the delta nose D. 138,538 8/1944 Clerc .................................. D12/331 wing and nose strake. There are eight pairs of control D. 155,569 10/1949 Bailey ............ ... D12/331 surfaces including an upper body stabilizer system for 3,447,76 6/1969 Whitener et al. ..................... 244/5 the control and stability of the airplane. -
Water-Tunnel and Analytical Investigation of the Effect of Strake
https://ntrs.nasa.gov/search.jsp?R=19800019803 2020-03-21T17:02:56+00:00Z NASA TP " 1676 NASA Technical Paper 1676 ,.,I c. 1 Water-Tunneland Analytical Investigation of the Effect of Strake Design Variables on Strake VortexBreakdown. Characteristics Neal T. Frink and John E. Lamar AUGUST 1980 TECH LIBRARY KAFB, NM NASA Technical Paper 1676 Water-Tunnel andAnalytical Investigation of the Effect of Strake Design Variables on Strake VortexBreakdown Characteristics Neal T. Frink andJohn E. Lamar Lavzgley Research Cetzter Haznptorz, Virgivzia National Aeronautics and Space Administration Scientific and Technical Information Branch 1980 SUMMARY A systematic water tunnel study was made to determine the vortex breakdown characteristics of43 strakes, more than half of which were generated from a new analytical strake design method. The strakes were mountedon a l/2-scale model of a Langley Research Center general research fighter fuselage mode1 with a 44O leading-edge-sweep trapezoidal wing. This study develops, in conjunction with a common wing-body, a parametric set of strake data for use in establishing and verifying a new strake design procedure. To develop this parametric data base, several series of isolated strakes were designedon the basis of a simplified approach which relates pre- scribed suction and pressure distributions in a simplified flow field to plan- form shapes. The resulting planform shapes provided examples of the effects of the pri- mary design parameters of size, span, and slenderness on the vortex breakdown characteristics. These effects are analyzed in relation to the respective strake leading-edge suction distributions. Included are examples of the effects of detailed strake planform shaping for strakes with the same general size and slenderness. -
Die Hohe Schule Des Segelfluges 145 Mehr Abnahm, Ja Am Fuße Des Stuifen Fast Null Wurde
AITH IE OE SCUE ES SEGEUGES EAG KA GI. EI W Kasigs ugecisce Sammug a ie oe Scue es Segeuges o W O 1 eie e Segeiegescue oeg i Wüemeg Eie Aeiug um emisce Woke- u Gewie-Segeug Mi eiäge o oma ima aa eisc Goeo Koe Maye u aee ekae Segeiege Mi 5 Aiuge 3 eessee u eweiee Auage eag Kasig Co G m . ei W 9 Coyig y Kasig e Co. G. m. ., ei. Ae ece, eisc. as e Ueeseug oeae. eeis is oisce üese, saisce Ueeseug i oeeiug. Dr. Friedrich Wenk, meiem eue eae ie i em uc eaee eicuge sowie as gewime Umscagi si egese o S. Wee, ei. uck o Ca Küge, Myau i.. Iaseeicis Seie orwort 8 Vorwort zur 3. Auflage 9 Einleitung 11 Flugbewegungen 13 Kurvenflug — Ludwig Hofmann 14 1. Fluggerät 20 Instrumente — Flugzeuge 2. Flug mit dem Frontgewitter 26 Mein erster Gewitterflug — Robert Kronfeld 27 Groenhoffs 272 km Frontflug 38 3. Thermikflug 44 Entstehung — Der „Abendthermikflug" — Der Segel- flug in der „Tagesthermik" — Direkte Sonnenther- mik — Ablösung der Thermik — Thermik in den Tropen — Thermik im Winter — Windthermik Flying high — Wolf Hirth 66 Thermikflugerfahrungen — Ludwig Hofmann 72 Segelflüge über der Ebene — Otto Fuchs .. 76 Neue Segelflugerfahrungen besonders mit Schlepp- start — Peter Riedel 79 Einige Erfahrungen im thermischen Segelflug — Ahrial 85 Motorlos von der Rhön an die Mosel — Wolf Hirth 87 4. Wolkenflug 92 Wie ich Blindfliegen übte — Ludwig Hofmann . 98 ronfeld schafft Weltrekordhöhe durch Wolkenflug 99 Meine Wolkenflüge im Rhönwettbewerb 1932 — A. Mayer t 101 Wolkenflug — Wolf Hirth 108 ame270 kin über Land — W. -
Newsletter Ono 49 Autuiftd I983
"GC Newsletter oNo 49 AUtUIftD I983 . '. 11. NEMZETKOZI VITORLAzOREPOLO OLDTIMER RALLY 1983. VII. 23-VIII. 3. FARKASHEGY BIA MAGYARORSZAG CAPTIONS FOR PHOTOGRAPHS THE 11TH INTERNATIONAl, VINTAGE GLIDER RALLY Photos by Ken Crack and Jen~ Novako Left to Right - Top to Bottom. The Opening, which took place on the very spot of the. first flight of a glider in Hungary during 1930, at the Farkashegy glidir,g site. 1. The plaquette of the 11th International Rally designed by Mitter Imre's son and worn by all participants of the Rally. 2. General Kiss Lajos, the Rally's Chief Sponsor and Representative of the Hungarian Aero Clubo Mitter Imre, and Szepesi Joszef, Chief Organizer of the Rally. Chief of the Air Branch of the Hungarian Civil Defence Assn. Chief Secretary of the Hungarian Aero Club and former Fighter Commander. 3. C. Wills, Sabine Novak and a beautiful Hungarian girl. 40 Ken Crack and the VGCvs Swiss Cow Bell at the Monument and brass plaque to commemorate the first Hungarian Glider flight .0 a bungee launch with a Z~gling. The aluminium wings are off a high perforrrance sailplane designed by RubiJ( Erno. It was found that the thin aluminium skin was corrugated (in Junkers style) for torsional stiffnesso However the corrugations do not indicate interior ribs. The ribs occur under flat skin, after every 5th corrugation. 50 Part of the crowd at the opening. The British were touched to notice that the Monument was in the form of a V, which only means Victory in English and French. The Hungarians have used this sign to symbolize the glorious achiev"ements of their old pilots. -
4 INVENTOR 16%/6/S G
May 21, 1968 F. G., NEUBECK 3,384,326 AERODYNAMIC STRAKE Filed Aug. 24, 1965 - E - - 4 INVENTOR 16%/6/s G. MazMayaea ... it is ATTORNEYsa 3,384,326 United States Patent Office Patented May 21, 1968 1. 2 bination of parts involved in the embodiment of the inven 3,384,326 tion as will appear from the following description and AERODYNAMC STRAKE accompanying drawings, wherein: Francis G. Neubeck, Eglin Air Force Base, Fla. FIG. 1 is a front elevation of the airplane showing the (94.67 Somerset Lane, Cypress, Calif. 90630) 5 angular relationship of the strakes in relation to the ver Filed Aug. 24, 1965, Ser. No. 482,304 tical axis of the airplane; 1 Claim. (CI. 244-13) FIG. 2 is a side elevation of the airplane showing the longitudinal position of a strake; FIG. 3 is an enlarged view of the rear portion of FIG. ABSTRACT OF THE DISCLOSURE 2, and showing with greater clarity the relationship be An elongated aerodynamic strake for use on an air 0 tween the aerodynamic strake and well-known airplane plane, and being in the form of a pentahedral prominence elements; and in plan and joined to and extending from each lower FIG. 4 is an enlarged plan view of the strake only. quarter aft section of the fuselage between the trailing The aerodynamic strake 10, constituting this invention, edge of the wing and the leading edge of the horizontal 5 is joined to the exterior of the fuselage skin on airplane stabilizer to be in the upwash area for improving overall 12, as shown on FIG. -
A Glider Pilot Bold... Wally Kahn a Glider Pilot Bold
A Glider Pilot Bold.. f ttom % fRfltng liBttattg of A Glider Pilot Bold... Wally Kahn A Glider Pilot Bold... Wally Kahn First edition published by Jardine Publishers 1998 Second edition published by Airplan Flight Equipment Ltd Copyright ©2008 Third edition published by Walter Kahn 2011 Copyright ©WALTER KAHN (1998 & 2008) and Airplan Flight Equipment (2008) WALTER KAHN 2011 All rights reserved. No part of this publication may be reproduced, stored in a retrieval system, or transmitted in any form, or by any means, electronic, mechanical, photocopying, recording or otherwise, without the prior permission of the publisher, except by a reviewer who wishes to quote brief passages in connection with a review written for inclusion in a newspaper, magazine, or radio or television broadcast. Every effort has been made by the author and the publishers to trace owners of copyright material. The events described have been cross-checked wherever possible and the author apologises for any errors or omissions which may have arisen. Cover photograph courtesy Neil Lawson. White Planes Co A Glider Pilot Bold... 1st Edition original cover Contents Another bite of the cherry .................................................................................9 Chapter 1 The early days and Oerlinghausen ..........................................15 Chapter 2 More Oerlinghausen.................................................................19 Chapter 3 Mindeheide and Scharfholdendorf ...........................................29 Chapter 4 Dunstable and Redhill -
May 1983 Issue of Soaring Magazine
Cambridge Introduces The New M KIV NA V Used by winners at the: 15M French Nationals U.S. 15M Nationals U.S. Open Nationals British Open Nationals Cambridge is pleased to announce the Check These Features: MKIV NAV, the latest addition to the successful M KIV System. Digital Final Glide Computer with • "During Glide" update capability The MKIV NAV, by utilizing the latest Micro • Wind Computation capability computer and LCD technology, combines in • Distance-to-go Readout a single package a Speed Director, a • Altitude required Readout 4-Function Audio, a digital Averager, and an • Thermalling during final glide capability advanced, digital Final Glide Computer. Speed Director with The MKIV NAV is designed to operate with the MKIV Variometer. It will also function • Own LCD "bar-graph" display with a Standard Cambridge Variometer. • No effect on Variometer • No CRUISE/CLIMB switching The MKIV NAV is the single largest invest ment made by Cambridge in state-of-the-art Digital 20 second Averager with own Readout technology and represents our commitment Relative Variometer option to keeping the U.S. in the forefront of soar ing instrumentation. 4·Function Audio Altitude Compensation Cambridge Aero Instruments, Inc. Microcomputer and Custom LCD technology 300 Sweetwater Ave. Bedford, MA 01730 Single, compact package, fits 80mm (31/8") Tel. (617) 275·0889; TWX# 710·326·7588 opening Mastercharge and Visa accepted BUSINESS. MEMBER G !TORGLIDING The JOURNAL of the SOARING SOCIETYof AMERICA Volume 47 • Number 5 • May 1983 6 THE 1983 SSA INTERNATIONAL The Soaring Society of America is a nonprofit SOARING CONVENTION organization of enthusiasts who seek to foster and promote all phases of gliding and soaring on a national and international basis.