The Voisin Biplane by Robert G
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MS – 204 Charles Lewis Aviation Collection
MS – 204 Charles Lewis Aviation Collection Wright State University Special Collections and Archives Container Listing Sub-collection A: Airplanes Series 1: Evolution of the Airplane Box File Description 1 1 Evolution of Aeroplane I 2 Evolution of Aeroplane II 3 Evolution of Aeroplane III 4 Evolution of Aeroplane IV 5 Evolution of Aeroplane V 6 Evolution of Aeroplane VI 7 Evolution of Aeroplane VII 8 Missing Series 2: Pre-1914 Airplanes Sub-series 1: Drawings 9 Aeroplanes 10 The Aerial Postman – Auckland, New Zealand 11 Aeroplane and Storm 12 Airliner of the Future Sub-series 2: Planes and Pilots 13 Wright Aeroplane at LeMans 14 Wright Aeroplane at Rheims 15 Wilbur Wright at the Controls 16 Wright Aeroplane in Flight 17 Missing 18 Farman Airplane 19 Farman Airplane 20 Antoinette Aeroplane 21 Bleriot and His Monoplane 22 Bleriot Crossing the Channel 23 Bleriot Airplane 24 Cody, Deperdussin, and Hanriot Planes 25 Valentine’s Aeroplane 26 Missing 27 Valentine and His Aeroplane 28 Valentine and His Aeroplane 29 Caudron Biplane 30 BE Biplane 31 Latham Monoplane at Sangette Series 3: World War I Sub-series 1: Aerial Combat (Drawings) Box File Description 1 31a Moraine-Saulnier 31b 94th Aero Squadron – Nieuport 28 – 2nd Lt. Alan F. Winslow 31c Fraser Pigeon 31d Nieuports – Various Models – Probably at Issoudoun, France – Training 31e 94th Aero Squadron – Nieuport – Lt. Douglas Campbell 31f Nieuport 27 - Servicing 31g Nieuport 17 After Hit by Anti-Aircraft 31h 95th Aero Squadron – Nieuport 28 – Raoul Lufbery 32 Duel in the Air 33 Allied Aircraft -
R/C Model for F3A Competition Biplane
5&PRGHO)RU)$FRPSHWLWLRQ%LSODQH (3)$PRWRU (3 1M23Z06706 Thank you for purchasing Futaba Sky Leaf R/C airplane. To maximize your enjoyment, and to ensure proper flying, please read through this assembly instruction manual. This product is for F3A competition. It can not be assembled or flighted by a beginner. It can be manufactured only for flyers with special skills. )XWDEDJXDUDQWHHVWKLVNLWWREHIUHHIURPGHIHFWVLQERWKPDWHULDODQG ZRUNPDQVKLS DW GDWH RI SXUFKDVH 7KLVZDUUDQW\GRHVQRWFRYHUDQ\ FRPSRQHQW SDUWVGDPDJHGE\XVHRUPRGLrFDWLRQ,QQRFDVHVKDOO)XWDEDOLDELOLW\H[FHHGWKH RULJLQDOFRVWRIWKHSXUFKDVHGNLW)XUWKHU)XWDEDUHVHUYHVWKHULJKWWRFKDQJHRU PRGLI\WKLVZDUUDQW\ZLWKRXWQRWLFH ,Q WKDW )XWDED KDV QR FRQWURO RYHU WKH ILQDO DVVHPEO\ RU PDWHULDO XVHG IRU ILQDO DVVHPEO\QROLDELOLW\VKDOOEHDVVXPHGQRUDFFHSWHGIRUDQ\GDPDJHUHVXOWLQJIURP WKH XVH E\ WKH XVHU RI WKH rQDO XVHUDVVHPEOHG SURGXFW %\ WKH DFW RI XVLQJ WKH XVHUDVVHPEOHGSURGXFWWKHXVHUDFFHSWVDOOUHVXOWLQJOLDELOLW\,IWKHEX\HULVQRW SUHSDUHGWRDFFHSWWKHOLDELOLW\DVVRFLDWHGZLWKWKHSURGXFWWKHEX\HULVDGYLVHGWR UHWXUQWKLVNLWLPPHGLDWHO\LQQHZDQGXQXVHGFRQGLWLRQWRWKHSODFHRISXUFKDVH Precautions ŤƓƓƏƌƆƄƗƌƒƑŃƄƑƇŃƐƒƇƌƲƆƄƗƌƒƑŃƓƕƈƆƄƘƗƌƒƑƖő 1. This product is only designed for use with radio control models. Use of the product described in this instruction manual is limited to radio control models. 2. Modification, adjustment, and parts replacement: Futaba is not responsible for unauthorized modification, adjustment, or replacement of parts on this product. 3. Your Sky Leaf should not be considered a toy, but rather a sophisticated, working model that functions very much like a full- size airplane. Because of its performance capabilities, this airplane, if not assembled and operated correctly, could possibly cause injury to yourself or spectators and damage to property. 4. You must assemble the model according to the instructions. Do not alter or modify the model, as doing so may result in an unsafe or unflyable model. In a few cases the instructions may differ slightly from the figures. -
A Numerical Approach for Implementing Air Intakes in a Canard Type Aircraft for Engine Cooling Purposes
https://doi.org/10.1590/jatm.v13.1192 ORIGINAL PAPER A Numerical Approach for Implementing Air Intakes in a Canard Type Aircraft for Engine Cooling Purposes Odenir de Almeida1,* , Pedro Correa Souza1 , Erick Cunha2 1.Universidade Federal de Uberlândia – Faculdade de Engenharia Mecânica – Centro de Pesquisa em Aerodinâmica Experimental – Uberlândia/MG – Brazil. 2.Fábrica Brasileira de Aeronaves – Uberlândia/MG – Brazil *Corresponding author: [email protected] ABSTRACT This work presents selected results of an unconventional aircraft development campaign. Engine installation at the rear part of the fuselage imposed design constraints for air intakes that should be used for cooling purposes. Trial and error flight tests increased the development cost and time which required a more sophisticated analysis through computational fluid dynamics (CFD) techniques and robust semiempirical approach. The carried-out investigation of the air intakes started with an empirical approach from guidelines for designing NACA and scoops. Numerical studies via computational fluid dynamics were performed with the air intakes installed in the aircraft fuselage. An analysis based on the air intake efficiency, drag and the effect of angle of attack are detailed in this work. Different air intakes designs, such as scoops of different shapes, were evaluated seeking for improved air intake efficiency and low drag while providing enough air for cooling the engine compartment. The results showed that the numerical approach used herein decreased the development cost and time of the aircraft, providing a reasonable low-cost approach and leading to a design selection more easily. Based on the current approach the canard airplane geometry was changed to account for the new selected air intake for engine cooling purposes. -
1908-1909 : La Véritable Naissance De L'aviation
1908-1909 : LA VÉRITABLE 05 Histoire et culture NAISSANCE DE L’AVIATION. de l’aéronautique et du spatial A) Les démonstrations en France de Farman et des frères Wright. A la veille de 1908, ballons et dirigeables dominent encore le ciel, malgré les succès prometteurs des frères Wright, de Santos Dumont et de Vuia. A Issy-les-Moulineaux, le 13 janvier 1908, Farman réussit officiellement le premier vol contrôlé en circuit fermé d’un kilomètre à bord d’un Voisin et remporte les 50 000 francs promis par Archdeacon et Deutsch de la Meurthe. Farman effectue ensuite le premier vol de ville à ville, entre Bouy et Reims, soit 27 km. En tournée aux Etats-Unis, il invente le mot “aileron” : il baptise ainsi les volets en bout d'aile d'avions qui sont présentés. Le premier passager de l'histoire de l'aviation serait Ernest Archdeacon qui embarque avec Henri Farman à Gand (Belgique). En août 1908, les frères Wright s’installent en France pour vendre leur « Flyer » sous licence. Le 31 décembre, Wilbur remporte les 20 000 francs du prix Michelin pour avoir effectué le plus long vol de l’année au camp d’Auvours : 124,7 km en 2h20. Les Wright voulaient garder secret leur système de gauchissement des ailes (torsion du bout des ailes pour incliner de côté un avion) au point de dormir à côté de l’avion. Les Américains fondent la première école de pilotage au monde à Pau. Aux Etats-Unis, le Wright Flyer III, piloté par Orville Wright, est victime d'un accident à la suite de la rupture d'une des hélices en plein vol. -
Flânerie Au Cœur Du Quartier Coteaux/Bords De Seine
Flânerie au cœur du quartier COTEAUX/BORDS DE SEINE 2km 1h30 www.saintcloud.fr Flânerie au cœur du quartier COTEAUX/BORDS DE SEINE Fière de son histoire et de son patrimoine, seuses au XIXe siècle. Le quai Carnot était la municipalité de Saint-Cloud vous invite également investi d’hôtels et restaurants à flâner dans les rues de la commune en qui accueillaient les Parisiens venus profi- publiant cinq livrets qui vous feront décou- ter des distractions organisées dans le parc vrir le patrimoine historique, artistique et de Saint-Cloud. Ce quartier devient plus architectural des différents quartiers de résidentiel au début du XXe siècle lorsque la Saint-Cloud. Le passionné de patrimoine Société foncière des Coteaux et du bois de ou l’amateur de belles promenades pourra Boulogne acquiert les terrains situés entre cheminer, de manière autonome, à l’aide les deux voies de chemin de fer. de ce dépliant, en suivant les points numé- rotés sur le plan (au verso) qui indique les Parcours de 2 kilomètres lieux emblématiques de la ville. Durée : environ 1h30 Partez à la découverte des vestiges, des En savoir plus sites classés ou remarquables qui vous Musée des Avelines, musée d’art révèleront la richesse de Saint-Cloud. Son et d’histoire de Saint-Cloud histoire commence il y a plus de 2000 ans 60, rue Gounod lorsque la ville n’était encore qu’une simple 92210 Saint-Cloud PARUTION JUILLET 2017 bourgade gallo-romaine appelée Novigen- 01 46 02 67 18 www.musee-saintcloud.fr tum. Entrée libre Le quartier des Coteaux, autrefois agricole, du mercredi au samedi de 12h à 18h vivait de la culture de la vigne tandis que Dimanche de 14h à 18h les bords de Seine étaient plutôt réservés Le musée organise des visites guidées à l’activité des pêcheurs puis des blanchis- de la ville. -
Aerodynamic Optimization of a Biplane Configuration Using Differential Evolution
Computer Aided Optimum Design in Engineering X 209 Aerodynamic optimization of a biplane configuration using differential evolution R. W. Derksen & A. G. Kraj Department of Mechanical and Manufacturing Engineering, University of Manitoba, Winnipeg, Manitoba, Canada Abstract This paper presents our work on designing a biplane configuration that has a minimum drag to lift ratio. This problem is a mixed optimization problem in that both discrete and continuous variables are used. Fourteen parameters were used to fully describe the biplane configuration and calculate performance. Performance calculations were based on Munk’s general biplane theory. Each wing required six parameters; airfoil profile type, span, tip and root chord lengths, angle of attack, and sweep angle. Two parameters were used to define the horizontal stagger and vertical gap between the two planes. The airfoil profile types were stored in an indexed database which allowed us to obtain the section’s aerodynamic characteristics. Our analysis showed that differential evolution found the optimum solution quickly. The characteristics of the resultant optimum solution will be discussed in detail, along with our observations of how the process needs to be adjusted for optimum performance. Keywords: aerodynamic design, optimization, biplanes, aerodynamic configuration. 1 Introduction The following sections will provide a brief review of the state-of-the-art of aerodynamic optimization. This will be followed by a discussion of the advantages and disadvantages of the biplane configuration. The introductory comments will conclude with the motivation for doing this work. 1.1 The practice of aerodynamic optimization A quest for performance has been a key component in the development of aviation from the start. -
Hangar 9 Ultimate Manual
TM® WE GET PEOPLE FLYING 46% TOC Ultimate 10-300 ASSEMBLY MANUAL Specifications Wingspan ..........................................................................................100 in (2540 mm) Length ................................................................................................110 in (2794 mm) Wing Area.........................................................................................3310 sq in (213.5 sq dm) Weight ...............................................................................................40–44 lb (18–20 kg) Engine.................................................................................................150–200cc gas engine Radio ..................................................................................................6-channel w/15 servos Introduction Thank you for purchasing the Hangar 9® 46% TOC Ultimate. Because size and weight of this model creates a higher degree for potential danger, an added measure of care and responsibility is needed for both building and flying this or any giant-scale model. It’s important that you carefully follow these instructions, especially those regarding hinging and the section on flying. Like all giant-scale aerobatic aircraft, the Hangar 9® TOC Ultimate requires powerful, heavy-duty servos. Servos greatly affect the flight performance, feel and response of the model. To get the most out of your Ultimate, it’s important to use accurate, powerful servos on all control surfaces. In the prototype models, we used JR 8411 digital servos with excellent -
1914/1918 : Nos Anciens Et Le Développement De L' Aviation
1914/1918 : Nos Anciens et le Développement de l’aviation militaire René Couillandre, Jean-Louis Eytier, Philippe Jung 06 novembre 2018 - 18h00 Talence 1914/1918 : Nos Anciens et le développement de l’ aviation militaire Chers Alumnis, chers Amis, Merci d’être venus nombreux participer au devoir de mémoire que toute Amicale doit à ses diplômés. Comme toute la société française en 1914, les GADZARTS, à l’histoire déjà prestigieuse, et SUPAERO, née en 1909, ont été frappés par le 1er conflit mondial. Les jeunes diplômés, comme bien d’autres ont été mobilisés pour répondre aux exigences nationales. Le conflit que tous croyaient de courte durée s’est révélé dévoreur d’hommes : toute intelligence, toute énergie, toute compétence fut mise au service de la guerre. L’aviation naissante, forte de ses avancées spectaculaires s’est d’abord révélé un service utile aux armes. Elle a rapidement évolué au point de devenir indispensable sur le champ de bataille et bien au-delà, puis de s’imposer comme une composante essentielle du conflit. Aujourd’hui, au centenaire de ce meurtrier conflit, nous souhaitons rendre hommage à nos Anciens qui, avec tant d’autres, de façon anonyme ou avec éclat ont permis l’évolution exceptionnelle de l’aviation militaire. Rendre hommage à chacun est impossible ; les célébrer collectivement, reconnaître leurs sacrifices et leurs mérites c’est nourrir les racines de notre aéronautique moderne. Nous vous proposons pour cela, après un rappel sur l’ aviation en 1913, d’effectuer un premier parcours sur le destin tragique de quelques camarades morts au champ d’honneur ou en service aérien en les resituant dans leur environnement aéronautique ; puis lors d’un second parcours, de considérer la présence et l’apport d’autres diplômés à l’évolution scientifique, technique, industrielle ou opérationnelle de l’ aviation au cours de ces 4 années. -
Experience Early Aviation with Fully
REVIEW Maxford’s vintage- themed models look extremely authentic when they are in the air, although pilots EXPERIENCE EARLY will probably want to spring for the available optional pilot figures to more AVIATION WITH capably create a convincing scalelike profile. FULLY FUNCTIONING WATCH A VIDEO! WING WARPING Access additional Maxford USA 1/9 Rumpler Taube EP 64-Inch ARF content by visiting By Jon Barnes | [email protected] www.ModelAviation. Photos by the author com/bonuscontent. THERE IS NO DENYING the surfaces, which would in the the Etrich Taube. Why the logic behind man’s eager efforts future become the standard for seeming disparity? It is primarily to take to the sky in a flying almost all aircraft, was the yaw because, with no licensing fees, machine. Engineers of the early axis. at least 14 companies built vari- 20th century understandably Designed by Igo Etrich in 1909, ations of the initial design. The attempted to mimic the methods the Taube first flew in 1910. It two-seat Rumpler Taube ulti- used by birds to change direction would become the first mass-pro- mately proved to be the most and altitude. At least one early duced aircraft in Germany, and common type and thus most effort to imitate the eminently go on to be used for military pur- appropriately the subject of flexible tail and wing feathers of poses by several of the nations Maxford’s attention. a bird can be seen in a mono- embroiled that were in World Maxford USA’s propensity to plane known as the Taube. War I. -
K&W Model Airplanes 1/5-Scale
Fly Historical Works of Art... These 1/5-scale ARF R/C aircraft are finished to a level that impresses even skilled model builders. All aircraft are conventional balsa and plywood construction, covered with a heat shrink fabric from Solarfilm. Rigging wires are factory assembled to the proper length. Where applicable, metal engine cowls and complete pull-pull systems are included for the elevator, rudder and aileron controls. Main landing gear, tail struts and scale wheels are factory assembled. For static display only, a wooden dummy engine and 2-blade scale propeller with front plate are included. Where possible KAVAN hardware is used in the models. Assembly instructions, flying hints and scale documentation is in English. Some models also include a German instruction. Most of the work is completed at the factory as the "Kit content" pictures show. Wires, tumbuckles and assembly hardware are included but not shown. The other aircraft are finished to the same level. Display models are available by special order. Two levels Kit content Phönix D-III, Austria-Hungary of detail are offered, Ready Not for Flying (RNF) and Museum Quality (MQ). These models have no provisions for installing an R/C engine and radio system. Asian and American interior decorators are a major customer of the Display models (RNF). Please contact KAVAN for price and delivery. Three models are NOT available for R/C flight (ARF). KAVAN stocks these three models in the RNF version, K&W Model Airplanes 1/5-scale ARF Wright Flyer 1, Breguet CU-1, Voisin Biplane. Kit content Macchi M-7, Italy Kit content Ryan NYP, N-X-211, USA 108 www.kavanrc.com Page Index KWM Oldtimer 1/5 Phönix D-III Austria-Hungary KWM.0117AU Page 130 Morane Saulnier type L Morane Saulnier type H Bleriot XI Nieuport 17- C1 Antionette VII France KWM.0103FR Page 116 KWM.0135FR Page 112 KWM.0104FR Page 115 KWM.0107FR Page 124 KWM.0120FR Page 127 Spad XIII Voisin Biplane, RNF Breguet CU-1, RNF KWM.0113FR Page 120 KWM.0242FR Page 139 KWM.0240FR Page 139 Nieuport 17-C1 Bristol F2B R.A.F. -
William J. Hammer Collection
William J. Hammer Collection Mark Kahn, 2003; additional information added by Melissa A. N. Keiser, 2021 2003 National Air and Space Museum Archives 14390 Air & Space Museum Parkway Chantilly, VA 20151 [email protected] https://airandspace.si.edu/archives Table of Contents Collection Overview ........................................................................................................ 1 Administrative Information .............................................................................................. 1 Biographical/Historical note.............................................................................................. 2 Scope and Contents........................................................................................................ 3 Arrangement..................................................................................................................... 4 Names and Subjects ...................................................................................................... 4 Container Listing ............................................................................................................. 5 Series 1: Professional materials............................................................................... 5 Series 2: Photographs and other materials............................................................ 13 William J. Hammer Collection NASM.XXXX.0074 Collection Overview Repository: National Air and Space Museum Archives Title: William J. Hammer Collection Identifier: NASM.XXXX.0074 Date: -
The Bleriot Xi: a Study in Aerodynamics by Robert G
THE BLERIOT XI: A STUDY IN AERODYNAMICS BY ROBERT G. WALDVOGEL If you wished to study aerodynamics, you would only need to look at the very early aircraft designs, such as the Bleriot XI. There are no high bypass ratio turbofans, nor upper deck lounges, nor global positioning systems. Instead, the aircraft is a sheer expression of the design solutions needed to overcome the four forces of flight: lift, weight, thrust, and drag. One of these “studies” can be made at Cole Palen’s Old Rhinebeck Aerodrome in Rhinebeck, New York. The culmination of ten previous configurations built by Louis Bleriot, who had reinvested 60,000 French francs amassed during an automobile lamp manufacturing venture to develop a technologically successful airplane in a race with such names as the Wright Brothers, Henri Farman, Santos Dumont, and Glenn Curtiss, the Bleriot XI itself had become the world’s first practical monoplane. The Bleriot VII, providing its initial foundation, had appeared with a partially enclosed fuselage to house its single pilot; wings braced to a tubular cabane framework over the cockpit; a four-bladed, 50-hp Antoinette engine; a large, dual-elevon horizontal tail; a small rudder; and swivelable, independently-sprung wheels. Although it crashed on December 18, 1907, it had nevertheless provided the foundation for a later, definitive design. The Bleriot VIII, rapidly following, had retained the low-wing configuration, but had featured pivoting, wing tip ailerons and a tricycle undercarriage, each comprised of single wheels. Although the Bleriot IX had been a larger variant of the VIII, and the Bleriot X had introduced a pusher-propeller arrangement with triple canard rudders, these intermediate steps had offered little to the ultimate design and therefore had been quickly discarded.