The Origins of the First Powered, Man-Carrying Airplane
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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 -
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). -
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 -
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. -
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. -
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. -
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. -
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 -
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. -
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. -
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.