The Origins of the First Powered, Man-Carrying Airplane

Total Page:16

File Type:pdf, Size:1020Kb

The Origins of the First Powered, Man-Carrying Airplane The Origins of the First Powered, Man-carrying Airplane The Wright brothers' "Flyer" of 1903 was not just a lucky effort by two bicycle mechanics from Dayton but the outcome of an intensive program of research, engineering and testing by F. E. C. Culick n a series of flights on December 17, they would have to follow a systematic vated the efforts, and so it was natural 1903, Wilbur and Orville Wright program of research and engineering. that the earliest ideas always entailed I became the first to pilot a powered He summarized his view in a lecture he the use of flapping wings. Sir George airplane. As is well known, they had de­ gave in September, 1901, at a meeting of Cayley (in 1799) was the first to under­ signed and built the craft themselves. To the Western Society of Engineers: "The stand that manned flight would be more this day, however, the notion persists problems of land and water travel were easily achieved if the means of generat­ that the Wright brothers were essen­ solved in the 19th century because it was ing lift were separated from the means tially bicycle mechanics who more or possible to begin with small achieve­ of propulsion. less stumbled on their successful design. ments and gradually work up to our Cayley is recognized as the originator Even among aeronautical engineers ig­ present success. The flying problem was of the airplane. His designs and conclu­ norance of what the Wrights accom­ left over to the 20th century, because in sions were based on careful observa­ plished is widespread. In tracing the this case the art must be highly devel­ tions and experiments. He conceived the steps by which the brothers arrived at oped before any flight of any consider­ configuration now viewed as being con­ their success, and in building a model of able duration at all can be obtained." ventional: a body or fuselage supporting their 1903 "Flyer" for tests in a wind Four years later the Wrights would have one main wing, with horizontal and ver­ tunnel, I have come to recognize how a practical airplane. tical tails positioned aft. He sucessfully remarkable their achievements in re­ Their invention of the powered, man­ flew gliders, one of them large enough to search, engineering and testing were. carrying airplane happened partly as carry a boy on at least one occasion. Their work deserves to be set in a richer a natural development from the work Cayley himself never flew. Among his historical context. of others. To an extraordinary de­ many other notable contributions were On the day of the first flights the gree, however, the Wrights' own contri­ demonstrations that curved surfaces are brothers took turns as pilot. Wilbur was butions were crucial. Their technical better than flat ones for providing lift; the pilot on the fourth, last and longest achievements were stunning, particular­ the idea that lateral balance or stability flight of the day, staying aloft for 59 ly when one considers where the effort can be gained by giving the wing a dihe­ seconds. Nearly four years passed be­ to achieve human flight stood in 1899. dral angle, that is, making it with raised fore anyone else was able to fly for as tips, and the concept of employing a long as a minute, and even then the ma­ Four Pioneers horizontal tail to achieve longitudinal chine was not fully controllable. By that stability. time the Wrights had developed a ma­ The people trying to build flying ma­ What Cayley began to comprehend neuverable airplane capable of flying chines had followed several strategies. were the intimate connections between for more than an hour. Observations of the flight of birds moti- the geometry of an aircraft, the forces As late as 1908, when the Wrights first flew publicly, no one else yet understood the need for lateral control, much less the function of the vertical tail. There­ fore no one else could execute proper turns. No one else knew how to make propellers correctly. Above all, no one else had pursued a comparable pro­ gram: doing the necessary research, con­ structing his own aircraft and doing his own flying, so that he understood the entire problem. The Wrights were able to outstrip all the other people who were trying to fly because they recognized the problems that had to be faced and solved. The brothers began their work in 1899, when Wilbur was 32 and Orville WRIGHTS' FLYER OF 1903, portrayed at the left in a view from the left side and at the right was 28. Wilbur, who was the informal in views from above and in front, was the first powered, man-carrying airplane to fly success­ leader in much of the work, realized fully. Its most distinctive feature was the forward horizontal control surface. The twin vertical 86 © 1979 SCIENTIFIC AMERICAN, INC acting on it and its stability in flight. An is provided mainly by the smaller hori­ longitudinal stability. Moreover, he un­ airplane has a vertical plane of symme­ zontal surface, which is usually placed derstood how the tail worked and gave try passing through its longitudinal axis. at the rear as Cayley advocated. Lateral the first explanation of its function in Motions that do not deflect the craft in stability is the effect of many causes, in­ prod ucing stable flight. directions out of that plane are called cluding the dihedral angle of the wings Otto Lilienthal, a mechanical engi­ longitudinal motions. The commonest and the vertical tail. The designs of early neer working in Germany, made major motion is pitching, in which the nose flying machines often included a verti­ contributions that directly influenced moves up or down. Sideslip, roll about cal tail for steering, by analogy with the the Wrights. In 1889 he published a the longitudinal axis and yaw about the rudder of a ship. The true function of book, The Flight of Birds as the Basis for vertical axis are collectively called later­ the vertical tail as a contribution to sta­ the Art of Aviation. that contained the al motions. bility was not apparent until the work of results of extensive experiments he had The tendency of any object in steady the Wrights. carried out with the help of his brother. motion to return to its initial state fol­ The giant of early French aeronautics That work provided the first useful data lowing a disturbance is called stability. was Alphonse penaud. He was the first on the lift and drag of curved airfoils. There are two kinds of stability, longitu­ to use wound strip rubber to power a Lilienthal also experimented in gliding, dinal and lateral, corresponding to the propeller-driven model airplane. Inde­ beginning in 1891, and became the first · two classes of motions of an airplane. In pendently of Cayley he conceived of the successful hang-glider pilot. He tried a modern aircraft longitudinal stability horizontal tail as a means of achieving both monoplane and multiplane gliders tail could not be moved except when the pilot warped the wings to the Wrights, fulfilled the function now uniformly done with ailerons. make a turn. Flying prone, he achieved warping by means of wires Wilbur and Orville Wright built the entire airplane, including the gas­ attached to a hip cradle. Wing warping, which was an invention of oline engine and propellers, which they had to design from scratch. 87 © 1979 SCIENTIFIC AMERICAN, INC and was killed while testing a mono­ ity. Although they were able to design enthal's death in 1896 aroused their in­ plane. their gliders to generate sufficient lift, terest in the problem of flying. In May, In the U.S. the most serious student of they had great difficulty maintaining 1899, Wilbur wrote to the secretary of aeronautics during this period was Oc­ balance in flight. They understood that the Smithsonian Institution asking for a tave Chanute, an eminent civil engineer. achieving balance meant making the list of the available literature on flight. With his writings and his own experi­ center of lift coincide with the center of Among the items he decided to buy was ments he brought Lilienthal's work to gravity. The difficulty arises because the Chanute's book Progress in Flying Ma­ the U.S. Because of his age (he was 68 in center of lift moves if the attitude of the chines, written in 1894. After stud ying 1900) he did no flying himself. He had aircraft is disturbed, as by a gust. In a the book Wilbur wrote to Chanute, initi­ several proteges who tested his gliders hang glider the pilot can restore balance ating an exchange of letters that contin­ and their own designs. by shifting his position in order to move ued for nearly 10 years. For most of that Chanute designed a biplane glider his center of gravity and change the atti­ period Chanute was a source of both that represents the beginnings of mod­ tude of the aircraft. If this maneuver is information and encouragement to the ern aircraft. (The design has served re­ accomplished correctly and consistent­ Wrights. The letters and the diaries of cently as the basis for several hang glid­ ly, the combination of the glider and the the Wrights constitute a detailed chroni­ ers.) Chanute adopted Penaud's aft tail pilot forms a stable system. cle from which one can reconstruct the for longitudinal stability, and for better When an aft horizontal tail is properly events leading to powered flight. lift he designed a cambered wing section installed, it will (as Penaud understood) similar to one tested by Lilienthal.
Recommended publications
  • 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
    [Show full text]
  • Modeling an Airframe Tutorial
    EAA SOLIDWORKS University p 1/11 Modeling an Airframe Tutorial Difficulty: Intermediate | Time: 1 hour As an Intermediate Tutorial, it is assumed that you have completed the Quick Start Tutorial and know how to sketch in 2D and 3D. If you struggle to recall how to do basic functions, please review the Tips Sheet. The Modeling an Airframe Tutorial guides you through the creation of a tubular airframe in SOLIDWORKS. The objective of the lesson is to teach you how to use the tools to design an aircraft frame. Time limits prevent us from completing this airframe, but you should learn the skills to model an airframe. You will create this part and drawing: This lesson includes: Creating a 3D Sketches Using the Weldment feature to add structural members Trimming structural members Creating a drawing and adding a ‘cut list’ Bill of Materials (BoM) EAA SOLIDWORKS University p 2/11 Modeling an Airframe Tutorial Creating a 3D Sketch for the Airframe In this lesson we will use the weldment feature to create an airframe. Weldments are structural members defined by a cross section picked from a library and a sketch line to define its length. This sketch line can be from multiple 2D sketches, or a single 3D sketch. By using two layout sketches (side and plan elevations), you can control the 3D sketch easily and any future changes will be reflected in your airframe. The layout sketches capture the design intent and the dimensions of the finished frame. 1. Open a New Part, verify Units are inches, and Save As “Airframe” (Top Menu / File / Save As).
    [Show full text]
  • 32 ROMANIAN CONTRIBUTIONS in AERONAUTICS Adrian NECULAE
    ROMANIAN CONTRIBUTIONS IN AERONAUTICS Adrian NECULAE West University of Timisoara, ROMANIA A short history of the flight From the earliest days, humans have dreamed of flying and have attempted to achieve it. The dream of flight was inspired by the observation of the birds even from the early times and was illustrated in myths, fiction (fantasy, science fiction and comic book characters) and art. Greek, Roman or Indian mythology have examples of gods who were gifted with flight. Daedalus and Icarus flew through the air, and Icarus died when he flew too close to the sun. Daedalus and Icarus (Greek) Pushpaka Vimana of the Ramayana (Indian) Religions relate stories of chariots that fly through the air and winged angels that join humans with the heavens. Flying creatures that were half human and half beast appear in legends. Birds and fantastic winged creatures pulled boats and other vehicles through the air. Let’s see some relevant examples: 32 From the top left corner: Angel, Pegasus, Dragons, Superman, Santa Claus, Dumbo. My talk is about progress in science, and more specific, about progresses in human fight against gravity. An illustration in art of the idea of what it means the progress in flight is given in the picture below, painted at the end of the 19th Century: The human dream of flight: Utopian flying machines from the 18th Century. The image and the title of this art work express, maybe better than other words, the idea of progress in flight, especially in modern and present history: things that seemed to be pure utopia a century
    [Show full text]
  • 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.
    [Show full text]
  • PC-6/B2-H4 Airplane Flight Manual Doc. No. 1820 at Revision 8
    PILOT’S INFORMATION MANUAL PC-6/B2-H4 applicable from AC S/N 825 PILOT’S INFORMATION MANUAL PC-6/B2-H4 applicable from AC S/N 825 WARNING •This PC-6 Pilot’s Information Manual is published for general and familiarization purposes only. •This Pilot’s Information Manual does NOT meet FAA, FOCA or any other civil aviation authority regulations for operation of ANY Aircraft. •This Pilot’s Information Manual is a reproduction of a PC-6 Airplane Flight Manual, however, it is NOT revised or updated. •This Pilot’s Information Manual does NOT reflect the configuration or operating parameters of any actual aircraft. •Only the Approved Airplane Flight Manual issued for a specific serial number aircraft may be used for actual operation of that serial number aircraft. Pilatus Aircraft Ltd P.O. Box 992 6371 Stans, Switzerland Phone +41 41 619 67 00 Fax +41 41 619 92 00 [email protected] www.pilatus-aircraft.com AIRPLANE FLIGHT MANUAL PC-6/B2-H4 ONLY REPORT NO. 1820 PURPOSES REGISTRATION ._____ __. SERIAL NO . APPLICABLE FROM A/C SIN 825 FAMILIARIZATION THIS AIRPLANDANE IS TO BE OPERAT ED IN COMPLIANCE WITH INFORMATION AND LIMI TATIONS CONTAINED HEREIN THIS FLIGHT MANUAL IS TO BE KEPT GENERAL IN THE AIRCRAFT AT ALL TIMES FOR Approved by: SWISS FEDERAL OFF FOR CIVIL AVIATION · �L Nov 20, JS�S" Date of Approval : ____·- ______ PILATUS AIRCRAFT LTD STANS/SWITZERLAND ONLY PURPOSES FAMILIARIZATION AND GENERAL FOR © Pilatus Aircraft Ltd. This document contains proprietary information that is protected by copyright. All rights are reserved, No part of this document may be copied, reproduced or translated to other languages without the prior written consent of Pilatus Aircraft Ltd.
    [Show full text]
  • Unit-1 Notes Faculty Name
    SCHOOL OF AERONAUTICS (NEEMRANA) UNIT-1 NOTES FACULTY NAME: D.SUKUMAR CLASS: B.Tech AERONAUTICAL SUBJECT CODE: 7AN6.3 SEMESTER: VII SUBJECT NAME: MAINTENANCE OF AIRFRAME AND SYSTEMS DESIGN AIRFRAME CONSTRUCTION: Various types of structures in airframe construction, tubular, braced monocoque, semimoncoque, etc. longerons, stringers, formers, bulkhead, spars and ribs, honeycomb construction. Introduction: An aircraft is a device that is used for, or is intended to be used for, flight in the air. Major categories of aircraft are airplane, rotorcraft, glider, and lighter-than-air vehicles. Each of these may be divided further by major distinguishing features of the aircraft, such as airships and balloons. Both are lighter-than-air aircraft but have differentiating features and are operated differently. The concentration of this handbook is on the airframe of aircraft; specifically, the fuselage, booms, nacelles, cowlings, fairings, airfoil surfaces, and landing gear. Also included are the various accessories and controls that accompany these structures. Note that the rotors of a helicopter are considered part of the airframe since they are actually rotating wings. By contrast, propellers and rotating airfoils of an engine on an airplane are not considered part of the airframe. The most common aircraft is the fixed-wing aircraft. As the name implies, the wings on this type of flying machine are attached to the fuselage and are not intended to move independently in a fashion that results in the creation of lift. One, two, or three sets of wings have all been successfully utilized. Rotary-wing aircraft such as helicopters are also widespread. This handbook discusses features and maintenance aspects common to both fixed wing and rotary-wing categories of aircraft.
    [Show full text]
  • AMA FPG-9 Glider OBJECTIVES – Students Will Learn About the Basics of How Flight Works by Creating a Simple Foam Glider
    AEX MARC_Layout 1 1/10/13 3:03 PM Page 18 activity two AMA FPG-9 Glider OBJECTIVES – Students will learn about the basics of how flight works by creating a simple foam glider. – Students will be introduced to concepts about air pressure, drag and how aircraft use control surfaces to climb, turn, and maintain stable flight. Activity Credit: Credit and permission to reprint – The Academy of Model Aeronautics (AMA) and Mr. Jack Reynolds, a volunteer at the National Model Aviation Museum, has graciously given the Civil Air Patrol permission to reprint the FPG-9 model plan and instructions here. More activities and suggestions for classroom use of model aircraft can be found by contacting the Academy of Model Aeronautics Education Committee at their website, buildandfly.com. MATERIALS • FPG-9 pattern • 9” foam plate • Scissors • Clear tape • Ink pen • Penny 18 AEX MARC_Layout 1 1/10/13 3:03 PM Page 19 BACKGROUND Control surfaces on an airplane help determine the movement of the airplane. The FPG-9 glider demonstrates how the elevons and the rudder work. Elevons are aircraft control surfaces that combine the functions of the elevator (used for pitch control) and the aileron (used for roll control). Thus, elevons at the wing trailing edge are used for pitch and roll control. They are frequently used on tailless aircraft such as flying wings. The rudder is the small moving section at the rear of the vertical stabilizer that is attached to the fixed sections by hinges. Because the rudder moves, it varies the amount of force generated by the tail surface and is used to generate and control the yawing (left and right) motion of the aircraft.
    [Show full text]
  • 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.
    [Show full text]
  • 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
    [Show full text]
  • Glider Handbook, Chapter 2: Components and Systems
    Chapter 2 Components and Systems Introduction Although gliders come in an array of shapes and sizes, the basic design features of most gliders are fundamentally the same. All gliders conform to the aerodynamic principles that make flight possible. When air flows over the wings of a glider, the wings produce a force called lift that allows the aircraft to stay aloft. Glider wings are designed to produce maximum lift with minimum drag. 2-1 Glider Design With each generation of new materials and development and improvements in aerodynamics, the performance of gliders The earlier gliders were made mainly of wood with metal has increased. One measure of performance is glide ratio. A fastenings, stays, and control cables. Subsequent designs glide ratio of 30:1 means that in smooth air a glider can travel led to a fuselage made of fabric-covered steel tubing forward 30 feet while only losing 1 foot of altitude. Glide glued to wood and fabric wings for lightness and strength. ratio is discussed further in Chapter 5, Glider Performance. New materials, such as carbon fiber, fiberglass, glass reinforced plastic (GRP), and Kevlar® are now being used Due to the critical role that aerodynamic efficiency plays in to developed stronger and lighter gliders. Modern gliders the performance of a glider, gliders often have aerodynamic are usually designed by computer-aided software to increase features seldom found in other aircraft. The wings of a modern performance. The first glider to use fiberglass extensively racing glider have a specially designed low-drag laminar flow was the Akaflieg Stuttgart FS-24 Phönix, which first flew airfoil.
    [Show full text]
  • 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.
    [Show full text]
  • Aircraft Circulars National Advisory
    AIRCRAFT CIRCULARS NATIONAL ADVISORY coLaITTEE FOR AERONAUTICS 1o. 164 THE STIEGER ST. 4 LIGHT AIRPLANE (BRITISH) A Twin-Engine Four-Seat Low-Wing 0,-).bin Monoplane Washington May, 1932 NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS AIRCRAFT CIRCULAR NO. 164 THE STIEGER ST. 4 LIGHT AIRPLANE (BRITISH)* A Twin-Engine Four-Seat Low-Wing Cabin Monoplane The ST. 4 is a twin-engine low-wing monoplane of the full cantilever type. Great care has been taken to keep the aerodynamic design "clean," and in order to avoid too great interference between fuselage and wing roots, the latter have been brought down to a thin section, while simultaneously. the trailing edge near the body has been raised. (Figs. 1, 2, 3.) Structurally, this arrangement has been achieved, by continuing the top boom of . the wing spar right across the fuselage, while the upper wing sur- face has been gradually reduced in camber as the fuselage is approached. As this surface drops away from the top spar boom, the latter becomes exposed, and is faired over the portion, which extends from the surface of the wing to the side of the fuselage. The wing consists structurally of three portions, or rather of two portions and a variation of one of them. These are: the wing root, the middle portion, and the wing tip . The middle portion and the tip are of dissimilar construction, although they are permanently attached to- gether, while the wing root, permanently attached to the fuselage and, indeed, forming an integral part of it, shows a type of construction quite different from both the middle and the end portions of the wing.
    [Show full text]