May 1983 Issue of Soaring Magazine
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STOL CH 701 / 750 Rudder Assembly Manual
STOL CH 701 / 750 Rudder Parts are labeled for easy identification with a part number and description: Part number example: 7R2-1 Rudder Spar 7 - STOL CH 701 model. R - Rudder section of the aircraft drawings. 2 - Page 2 of the Rudder drawings. 1 - Part 1 on page 2. Kit parts that make up the rudder skeleton. Drawing 7-R-0 is for reference only: for building sequence use this step by step photo assembly guide. This manual has been prepared for assembly of the Rudder Starter Kit supplied with the predrilled Rudder Spar, (starting May 2007), and match drilled Bottom Rib, (starting Jan. 2008). Previous versions did not include the predrilled Rudder Spar or match drilled Bottom Rib. In addition to the photo assembly guide, also refer to drawings 7-R-1, 7-R-2 and 7-R-3 (701) or 75-R-1, 75-R-2, and 75RA-1 (750) (drawing number in right bottom corner of the title block). Always refer to the drawings for technical information: material thickness, part dimension, part orientation, layout distances, and rivet sizes, location and spacing. STOL Zenith Aircraft Company Revision 1.7 (02/2010) RUDDER SKELETON, 7-R-2 CH 701 / 750 www.zenithair.com © 2005 Zenith Aircraft Co SECTION 1 - Page 1 of 12 7R2-1 Spar or 75R2-3 Spar Spar Web - term used to refer to the flat area between the flanges. Tool: half round 6” fine (smooth) double cut hand file. Use a file to remove any burs on the edges of the parts and lightly round off corners. -
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. -
Guide to the Paul Maccready Innovative Lives Presentation
Guide to the Paul MacCready Innovative Lives Presentation NMAH.AC.0842 Alison Oswald 2003 Archives Center, National Museum of American History P.O. Box 37012 Suite 1100, MRC 601 Washington, D.C. 20013-7012 [email protected] http://americanhistory.si.edu/archives Table of Contents Collection Overview ........................................................................................................ 1 Administrative Information .............................................................................................. 1 Scope and Contents........................................................................................................ 2 Biographical / Historical.................................................................................................... 2 Names and Subjects ...................................................................................................... 2 Container Listing ............................................................................................................. 3 Series : Original Videos (OV 842.1-9), 2002-11-08................................................. 3 Series : Reference Videos, 2002-11-08................................................................... 4 Series 3: Digital images, 2002-11-08....................................................................... 5 Paul MacCready Innovative Lives Presentation NMAH.AC.0842 Collection Overview Repository: Archives Center, National Museum of American History Title: Paul MacCready Innovative Lives Presentation Identifier: -
Helicopter Dynamics Concerning Retreating Blade Stall on a Coaxial Helicopter
Helicopter Dynamics Concerning Retreating Blade Stall on a Coaxial Helicopter A project presented to The Faculty of the Department of Aerospace Engineering San José State University In partial fulfillment of the requirements for the degree Master of Science in Aerospace Engineering by Aaron Ford May 2019 approved by Prof. Jeanine Hunter Faculty Advisor © 2019 Aaron Ford ALL RIGHTS RESERVED ABSTRACT Helicopter Dynamics Concerning Retreating Blade Stall on a Coaxial Helicopter by Aaron Ford A model of helicopter blade flapping dynamics is created to determine the occurrence of retreating blade stall on a coaxial helicopter with pusher-propeller in straight and level flight. Equations of motion are developed, and blade element theory is utilized to evaluate the appropriate aerodynamics. Modelling of the blade flapping behavior is verified against benchmark data and then used to determine the angle of attack distribution about the rotor disk for standard helicopter configurations utilizing both hinged and hingeless rotor blades. Modelling of the coaxial configuration with the pusher-prop in straight and level flight is then considered. An approach was taken that minimizes the angle of attack and generation of lift on the advancing side while minimizing them on the retreating side of the rotor disk. The resulting asymmetric lift distribution is compensated for by using both counter-rotating rotor disks to maximize lift on their respective advancing sides and reduce drag on their respective retreating sides. The result is an elimination of retreating blade stall in the coaxial and pusher-propeller configuration. Finally, an assessment of the lift capability of the configuration at both sea level and at “high and hot” conditions were made. -
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. -
Soaring Club in Middletown, NY
contests. He flies at both Wurtsboro Airport and with Va lley Soaring Club in Middletown, NY. Ward received instruction fr om several instructors at Va lley Soaring and fr om Warren Cramer at Wu rtsboro Airport, and took his check-ride with examiner Wa lly Moran. Pictured are Wa rd (left), Wa rren research on soaring weather, and has (center), and Wally (right). been the weatherman fo r several gliding -Warren Cramer Kennedy (right). He successfully soloed his Grob- 103 on May 28, 2010, earning his SSA A badge. Rich quickly Ridge Soaring Gliderport earned hisSS A B badge only a fe w days later. Rich, shown here, soaking wet ---- Julian, Pennsylvania fr om the traditional, "wetting down" is congratu lated by his instrucrorJoel FOR SALE Te refenko. Rich is on track ro finishup his Private Pilot Certificate very soon as • Commercially licensed, world fa mous Gliderport near Penn State University. well as earninghis C and Bronze badges. (90 acres with state-stocked trout stream). -Phil Jones • 3600 ft grass runway 1500 ft paved portion. • Threehangars, office building,bunkhouse, workshop. Two tow planes. three ANEW CFI-G two-place gliders, one single-place glider, mowers, tractors and equipment. Ward Hindman passed his check-ride • Catalog business included. Tu rnkey, profitable business since 1975. on June 2, 201 0, at Wu rtsboro Airport, and is now a certi ficated glider flight instructor. Ward has been an active CALL 814-355-2483 glider pilot fo r many years, completed See web site fo r photos: www.eglider.org The gliding maga· zlne with the worl d· wide circulation that brings soaring news from 32 gliding na· tions . -
DR. PAUL MACCREADY September 29, 1925 - August 28, 2007 AMA #626304
The AMA History Project Presents: Biography of DR. PAUL MACCREADY September 29, 1925 - August 28, 2007 AMA #626304 Transcribed & Edited by SS (08/2002); Update by JS (02/2017) Career: . Set many model airplane records . First soloed in a powered plane at age 16 . Flew in the U.S. Navy flight-training program during World War II . 1947: Graduated with a Bachelor of Science degree in physics from Yale University . Won second place in the National Soaring Contest at Wichita Falls, Texas, at age 21 . 1948, 1949, 1953: Won the U.S. National Soaring Championships . Pioneered high-altitude wave soaring in the U.S. 1956: Became the first American to be an international sailplane champion at a meet in France; represented the U.S. in Europe four times . Invented the MacCready speed ring used worldwide by glider pilots . Earned his master’s degree in physics in 1948 and his doctorate degree in aeronautics in 1952, both from the California Institute of Technology . 1971: Started AeroVironment, Inc. Won a few Henry Kremer Prizes for his cutting-edge designs of planes, such as planes powered by human power only . Early 1980s: Developed solar-powered planes . Received various honors and awards and is affiliated with the National Academy of Engineering, the American Academy of Arts and Sciences, the American Institute of Aeronautics and Astronautics and the American Meteorological Society . Served as the international president of the International Human Powered Vehicle Association . Wrote many articles, papers and reports dealing with physics and aeronautics . 2016 AMA Model Aviation Hall of Fame inductee This biography, written in 1986, is stored in the AMA History Project (at the time called the AMA History Program) files. -
Jason Dunham Cmd Inv
DEPARTMENT OF THE NAVY UNITED STATES FLEET FORCES COMMAND 1562 MITSCHER AVENUE SUITE 250 NORFOLK VA 23551-2487 5830 SerN 00/15 1 7 May 19 FINAL ENDORSEMENT on bf(& ltr of27 Jul 18 From : Commander , U.S. Fleet Forces Command To: File Subj : COMNIAND INVESTIGATION INTO THE DEATH OF ENS SARAH JOY MITCHELL, USN , AT SEA ON 8 JULY 2018 Encl: (64) Voluntary Statement of 16R6 dtd 1 Apr 19 (65) Voluntary Statement of -----b){&) dtd 1 Apr 19 1. I thoroughly reviewed the subject investigation and its endorsements . I approve the findings of fact opinions , and recommendations as previously endorsed and as modified below. 2. Findings of Facts: a. FF 312 added: On the morning of 8 July=~-=--==-=-=,-,,-,:--e-=--==-=-=--=--~ was on the bridge prior to launchino RIB KELLY MILLER and RIB BILLY HAMPTON . After confening with the OOD bJl&J , ll>H& made the decision to execute planned RIB operations . [Encl (21)] b. FF 313 added: The OOD is cha1·ged with "the direct supervi sion of the ship's boats" and is responsible for "ensming that all boat safety regulations are observed" in accordance with reference (c). c. FF 314 added: lliR6 wa s the scheduled OOD for the 0700 - 0930 watch and assumed the watch at 0700. [Encl (17), (22), (64)] d. FF 3 15 added: The boat deck was given pennission from "6f( , thrnugh 6)l6J b)(&) , to load lower , and launch RIB KELLY MILLER and RIB BILLY HAMPTON. Both Rill s were in the water at approxima tely 0910. [Encl (17), (21) , (64)] gave u·ip and shove off orders to the two RIBs before breakaway and then gave them,------- pennission to load , lower and launch when they were rnady. -
Small Lightweight Aircraft Navigation in the Presence of Wind Cornel-Alexandru Brezoescu
Small lightweight aircraft navigation in the presence of wind Cornel-Alexandru Brezoescu To cite this version: Cornel-Alexandru Brezoescu. Small lightweight aircraft navigation in the presence of wind. Other. Université de Technologie de Compiègne, 2013. English. NNT : 2013COMP2105. tel-01060415 HAL Id: tel-01060415 https://tel.archives-ouvertes.fr/tel-01060415 Submitted on 3 Sep 2014 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. Par Cornel-Alexandru BREZOESCU Navigation d’un avion miniature de surveillance aérienne en présence de vent Thèse présentée pour l’obtention du grade de Docteur de l’UTC Soutenue le 28 octobre 2013 Spécialité : Laboratoire HEUDIASYC D2105 Navigation d'un avion miniature de surveillance a´erienneen pr´esencede vent Student: BREZOESCU Cornel Alexandru PHD advisors : LOZANO Rogelio CASTILLO Pedro i ii Contents 1 Introduction 1 1.1 Motivation and objectives . .1 1.2 Challenges . .2 1.3 Approach . .3 1.4 Thesis outline . .4 2 Modeling for control 5 2.1 Basic principles of flight . .5 2.1.1 The forces of flight . .6 2.1.2 Parts of an airplane . .7 2.1.3 Misleading lift theories . 10 2.1.4 Lift generated by airflow deflection . -
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. -
Artifacts and Aircraft
International Journal of Business, Humanities and Technology Vol. 5, No. 2; April 2015 The Ancients: Artifacts and Aircraft Susan Kelly Archer, EdD Embry-Riddle Aeronautical University Department of Doctoral Studies College of Aviation Daytona Beach, Florida USA Abstract Throughout literature and other art forms, certain themes appear repeatedly. The same might be said for engineering designs, specifically the design of aerospace vehicles. In 1996, Lumir Janku wrote about a set of artifacts, discovered in Peru and determined to be Pre-Columbian, that can be interpreted as models of delta- winged fliers. The design of the Peruvian artifacts has been interpreted in multiple ways by a variety of professionals. The delta wing was also incorporated into the design of civilian aircraft during the 20th Century. Modern delta-winged aircraft were used successfully in both military and civilian applications for more than 40 years. It is interesting to read about the possibility that this aeronautical design may have originated millennia earlier with a culture that did not leave written records to explain its artifacts crafted in gold. Keywords: aviation history, delta wing, Pre-Columbian artifacts Throughout literature and other art forms, certain themes appear repeatedly. The same might be said for engineering designs, specifically the design of aerospace vehicles. Man’s fascination with how birds fly can be linked to the ancient legends of Daedalus or the winged Egyptian gods, and then more recently to John Damien’s attempt to fly with wings made from chicken feathers (Brady, 2000) or Otto Lillienthal’s essays linking the physiology of birds to the design of early gliders (Lillienthal, 2001). -
04 Delta Wings
ExperimentalExperimental AerodynamicsAerodynamics Lecture 4: Delta wing experiments G. Dimitriadis Experimental Aerodynamics Introduction •! In this course we will demonstrate the use of several different experimental aerodynamic methodologies •! The particular application will be the aerodynamics of Delta wings at low airspeeds. •! Delta wings are of particular interest because of their lift generation mechanism. Experimental Aerodynamics Delta wing history •! Until the 1930s the vast majority of aircraft featured rectangular, trapezoidal or elliptical wings. •! Delta wings started being studied in the 1930s by Alexander Lippisch in Germany. •! Lippisch wanted to create tail-less aircraft, and Delta wings were one of the solutions he proposed. Experimental Aerodynamics Delta Lippisch DM-1 Designed as an interceptor jet but never produced. The photos show a glider prototype version. Experimental Aerodynamics High speed flight •! After the war, the potential of Delta wings for supersonic flight was recognized both in the US and the USSR. MiG-21 Convair XF-92 Experimental Aerodynamics Low speed performance •! Although Delta wings are designed for high speeds, they still have to take off and land at small airspeeds. •! It is important to determine the aerodynamic forces acting on Delta wings at low speed. •! The lift generated by such wings are low speeds can be split into two contributions: –! Potential flow lift –! Vortex lift Experimental Aerodynamics Delta wing geometry cb Wing surface: S = 2 2b Aspect ratio: AR = "! c c! b AR Sweep angle: tan ! = = 2c 4 b/2! Experimental Aerodynamics Potential flow lift •! Slender wing theory •! The wind is discretized into transverse segments. •! The flow around each segment is modeled as a 2D flow past a flat plate perpendicular to the free stream Experimental Aerodynamics Slender wing theory •! The problem of calculating the flow around the wing becomes equivalent to calculating the flow around each 2D segment.