Was the Airplane an American Invention?
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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 -
A Short History of the Royal Aeronautical Society
A SHORT HISTORY OF THE ROYAL AERONAUTICAL SOCIETY Royal Aeronautical Society Council Dinner at the Science Museum on 26 May 1932 with Guest of Honour Miss Amelia Earhart. Edited by Chris Male MRAeS Royal Aeronautical Society www.aerosociety.com Afterburner Society News RAeS 150th ANNIVERSARY www.aerosociety.com/150 The Royal Aeronautical Society: Part 1 – The early years The Beginning “At a meeting held at Argyll Lodge, Campden Hill, Right: The first Aeronautical on 12 January 1866, His Grace The Duke of Argyll Exhibition, Crystal Palace, 1868, showing the presiding; also present Mr James Glaisher, Dr Hugh Stringfellow Triplane model W. Diamond, Mr F.H. Wenham, Mr James Wm. Butler and other exhibits. No fewer and Mr F.W. Brearey. Mr Glaisher read the following than 77 exhibits were address: collected together, including ‘The first application of the Balloon as a means of engines, lighter- and heavier- than-air models, kites and ascending into the upper regions of the plans of projected machines. atmosphere has been almost within the recollection A special Juror’s Report on on ‘Aerial locomotion and the laws by which heavy of men now living but with the exception of some the exhibits was issued. bodies impelled through air are sustained’. of the early experimenters it has scarcely occupied Below: Frederick W Brearey, Wenham’s lecture is now one of the aeronautical Secretary of the the attention of scientific men, nor has the subject of Aeronautical Society of Great classics and was the beginning of the pattern of aeronautics been properly recognised as a distinct Britain, 1866-1896. -
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. -
Federal Aviation Administration, DOT § 61.45
Federal Aviation Administration, DOT Pt. 61 Vmcl Minimum Control Speed—Landing. 61.35 Knowledge test: Prerequisites and Vmu The speed at which the last main passing grades. landing gear leaves the ground. 61.37 Knowledge tests: Cheating or other VR Rotate Speed. unauthorized conduct. VS Stall Speed or minimum speed in the 61.39 Prerequisites for practical tests. stall. 61.41 Flight training received from flight WAT Weight, Altitude, Temperature. instructors not certificated by the FAA. 61.43 Practical tests: General procedures. END QPS REQUIREMENTS 61.45 Practical tests: Required aircraft and equipment. [Doc. No. FAA–2002–12461, 73 FR 26490, May 9, 61.47 Status of an examiner who is author- 2008] ized by the Administrator to conduct practical tests. PART 61—CERTIFICATION: PILOTS, 61.49 Retesting after failure. FLIGHT INSTRUCTORS, AND 61.51 Pilot logbooks. 61.52 Use of aeronautical experience ob- GROUND INSTRUCTORS tained in ultralight vehicles. 61.53 Prohibition on operations during med- SPECIAL FEDERAL AVIATION REGULATION NO. ical deficiency. 73 61.55 Second-in-command qualifications. SPECIAL FEDERAL AVIATION REGULATION NO. 61.56 Flight review. 100–2 61.57 Recent flight experience: Pilot in com- SPECIAL FEDERAL AVIATION REGULATION NO. mand. 118–2 61.58 Pilot-in-command proficiency check: Operation of an aircraft that requires Subpart A—General more than one pilot flight crewmember or is turbojet-powered. Sec. 61.59 Falsification, reproduction, or alter- 61.1 Applicability and definitions. ation of applications, certificates, 61.2 Exercise of Privilege. logbooks, reports, or records. 61.3 Requirement for certificates, ratings, 61.60 Change of address. -
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. -
Efficient Light Aircraft Design – Options from Gliding
Efficient Light Aircraft Design – Options from Gliding Howard Torode Member of General Aviation Group and Chairman BGA Technical Committee Presentation Aims • Recognise the convergence of interest between ultra-lights and sailplanes • Draw on experiences of sailplane designers in pursuit of higher aerodynamic performance. • Review several feature of current sailplanes that might be of wider use. • Review the future for the recreational aeroplane. Lift occurs in localised areas A glider needs efficiency and manoeuvrability Drag contributions for a glider Drag at low speed dominated by Induced drag (due to lift) Drag at high ASW-27 speeds Glider (total) drag polar dominated by profile drag & skin friction So what are the configuration parameters? - Low profile drag: Wing section design is key - Low skin friction: maximise laminar areas - Low induced drag – higher efficiencies demand greater spans, span efficiency and Aspect Ratio - Low parasitic drag – reduce excrescences such as: undercarriage, discontinuities of line and no leaks/gaps. - Low trim drag – small tails with efficient surface coupled with low stability for frequent speed changing. - Wide load carrying capacity in terms of pilot weight and water ballast Progress in aerodynamic efficiency 1933 - 2010 1957: Phoenix (16m) 1971: Nimbus 2 (20.3m) 2003: Eta (30.8m) 2010: Concordia (28m) 1937: Wiehe (18m) Wooden gliders Metal gliders Composite gliders In praise of Aspect Ratio • Basic drag equation in in non-dimensional, coefficient terms: • For an aircraft of a given scale, aspect ratio is the single overall configuration parameter that has direct leverage on performance. Induced drag - the primary contribution to drag at low speed, is inversely proportional to aspect ratio • An efficient wing is a key driver in optimising favourable design trades in other aspects of performance such as wing loading and cruise performance. -
Fitzpatrick Biography
The James L. G. Fitz Patrick Papers Archives & Special Collections College of Staten Island Library, CUNY 2800 Victory Blvd., 1L-216 Staten Island, NY 10314 © 2005, 2018 The College of Staten Island, CUNY Finding Aid by James A. Kaser Overview of the Collection Collection No. : CM-4 Title: The James L. G. Fitz Patrick Papers Creator: James L. G. Fitz Patrick (1906-1998) Dates: c. 1926-1998 Extent: Approximately 1.5 Linear Feet Abstract: Prof. James L. G. Fitzpatrick was a faculty member and administrator at the Staten Island Community College from 1959 to 1976. He taught and served as Head of the Department of Mechanical Technology. He was appointed the first Academic Dean of the college in 1959, serving as Dean of the Faculty and acting under the college president to administer the academic program. He also coordinated a large part of the planning for the college’s campus in Sunnyside, completed in 1967. Fitz Patrick became Dean for Operations and Development in 1971 and held that position until his retirement in 1976. Fitz Patrick was widely recognized as an expert on natural flight and aeronautics. This fragmentary collection mostly documents some of Fitz Patrick’s research activities. Administrative Information Preferred Citation The James L. G. Fitz Patrick Papers, Archives & Special Collections, Department of the Library, College of Staten Island, CUNY, Staten Island, New York Acquisition The papers were donated by Fitz Patrick’s stepson, Harold J. Smith. Processing Information Collection processed by the staff of Archives & Special Collections. 1 Restrictions Access Access to this record group is unrestricted. -
Winter 2016 Issue No 128
The Oily Rag! Photo Peter Nicholson Tony Newberry surrounded by some of the locos he has built at a celebration of his achievements at Coate Water Miniature Railwa y Peter Nicholson and Joshua Brinsford report WinterWinter 2016 Issue No 128 TheThe Taunton Model Engineers’ magazinemagazine 1 ContentsContents 3. From the Editor 3. Chairman’s Notes 5. News from Creech 7. Report from Vivary Park 9. Steam powered aircraf t By William Pickering Do you believe this? 14. Robin No. 6 By Tim Griffiths Would you like to be involved with rebuilding this loco? 16. “On the footplate” The art of stopping By Ray Rolt Ray brings his experiences on the S&DR to a halt. 20. Tony Newberry honoured at Coate Miniature Railway A report by Peter Nicholson and Joshua Brinsfo rd 23. “Tich 2.5” By John Pickering A new take on a classic design. 25. Little puffers way By Tim Griffiths Tim’s early days in South London 28. Of ships and things By Fireman M.N. retired Clean clothes and black smoke 2 From the Editor Tony Newberry is probably our most prolific model engineer. On the weekend of the 13th and 14th August an event was held at the North Wilts Model Engineering Society’s Coate Water Miniature Railway to celebrate his achievements. Peter Nicholson and Joshua Brinsford report on this event. This issue has nostalgia with pieces from Tim Griffiths and fireman MN retd. Ray Rolt complet es his series on driving on the S&DR. appropriately with the “art of stopping”. To fill the pages I was able to call on a source from beyond the grave. -
Design of a Micro-Aircraft Glider
Design of A Micro-Aircraft Glider Major Qualifying Project Report Submitted to the faculty of WORCESTER POLYTECHNIC INSTITUTE In partial fulfillment of the requirements for The Degree of Bachelor of Science Submitted by: ______________________ ______________________ Zaki Akhtar Ryan Fredette ___________________ ___________________ Phil O’Sullivan Daniel Rosado Approved by: ______________________ _____________________ Professor David Olinger Professor Simon Evans 2 Certain materials are included under the fair use exemption of the U.S. Copyright Law and have been prepared according to the fair use guidelines and are restricted from further use. 3 Abstract The goal of this project was to design an aircraft to compete in the micro-class of the 2013 SAE Aero Design West competition. The competition scores are based on empty weight and payload fraction. The team chose to construct a glider, which reduces empty weight by not employing a propulsion system. Thus, a launching system was designed to launch the micro- aircraft to a sufficient height to allow the aircraft to complete the required flight by gliding. The rules state that all parts of the aircraft and launcher must be contained in a 24” x 18” x 8” box. This glider concept was unique because the team implemented fabric wings to save substantial weight and integrated the launcher into the box to allow as much space as possible for the aircraft components. The empty weight of the aircraft is 0.35 lb, while also carrying a payload weight of about 0.35 lb. Ultimately, the aircraft was not able to complete the required flight because the team achieved 50% of its desired altitude during tests. -
NASA Styrofoam Tray Glider.Pdf
RIGHT FLIGHT Objectives The students will: Construct a flying model glider. Determine weight and balance of a glider. Standards and Skills Science Science as Inquiry Physical Science Science and Technology Unifying Concepts and Processes Science Process Skills Observing Measuring Collecting Data Inferring Predicting Making Models Controlling Variables Mathematics Problem Solving Reasoning Prediction Measurement Background On December 17, 1903, two brothers, Wilbur and Orville Wright, became the first humans to fly a controllable, powered airplane. To unravel the mysteries of flight, the Wright brothers built and experimented extensively with model gliders. Gliders are airplanes without motors or a power source. 52 Aeronautics: An Educator’s Guide EG-2002-06-105-HQ Building and flying model gliders helped the Wright brothers learn and understand the importance of weight and balance in air- planes. If the weight of the airplane is not positioned properly, the airplane will not fly. For example, too much weight in the front (nose) will cause the airplane to dive toward the ground. The precise balance of a model glider can be determined by varying the location of small weights. Wilbur and Orville also learned that the design of an airplane was very important. Experimenting with models of different designs showed that airplanes fly best when the wings, fuselage, and tail are designed and balanced to interact with each other. The Wright Flyer was the first airplane to complete a controlled takeoff and landing. To manage flight direction, airplanes use control surfaces. Elevators are control surfaces that make the nose of the airplane pitch up and down. A rudder is used to move the nose left and right. -
Federal Aviation Administration, DOT § 91.313
Federal Aviation Administration, DOT § 91.313 (2) The towing aircraft is equipped light vehicle, in a manner that endan- with a tow-hitch of a kind, and in- gers the life or property of another. stalled in a manner, that is approved [Doc. No. 18834, 54 FR 34308, Aug. 18, 1989, as by the Administrator; amended by Amdt. 91–227, 56 FR 65661, Dec. (3) The towline used has breaking 17, 1991; Amdt. 91–282, 69 FR 44880, July 27, strength not less than 80 percent of the 2004] maximum certificated operating weight of the glider or unpowered § 91.311 Towing: Other than under ultralight vehicle and not more than § 91.309. twice this operating weight. However, No pilot of a civil aircraft may tow the towline used may have a breaking anything with that aircraft (other than strength more than twice the max- under § 91.309) except in accordance imum certificated operating weight of with the terms of a certificate of waiv- the glider or unpowered ultralight ve- er issued by the Administrator. hicle if— (i) A safety link is installed at the § 91.313 Restricted category civil air- point of attachment of the towline to craft: Operating limitations. the glider or unpowered ultralight ve- (a) No person may operate a re- hicle with a breaking strength not less stricted category civil aircraft— than 80 percent of the maximum cer- (1) For other than the special purpose tificated operating weight of the glider for which it is certificated; or or unpowered ultralight vehicle and (2) In an operation other than one not greater than twice this operating necessary to accomplish the work ac- weight; tivity directly associated with that (ii) A safety link is installed at the special purpose. -
An Ancient Air – John Stringfellow
AnAirlife CLASSIC AN ANCIENT AIR The invention all admired and each how he To be the inventor missed; so easy it seemed Once found, which yet unfound Most would have thought impossible. Milton BIOGRAPHY (JL THE VICTORIAN AERONAUTICAL HARALD PEMRUbfc AnAirlife CLASSIC Copyright © 1988 Harald Penrose First published in the UK in 1988 by Airlife Publishing Ltd This edition published 2000 British Library Cataloguing-in-Publication Data A catalogue record for this book is available from the British Library ISBN 1840371846 All rights reserved. No part of this book may be reproduced or transmitted in any form or by any means, electronic or mechanical including photocopying, recording or by any information storage and retrieval system, without permission from the Publisher in writing. Printed in England by St Edmundsbury Press Ltd, Bury St Edmunds, Suffolk Airlife Publishing Ltd 101 Longden Road, Shrewsbury, SYS 9EB, England E-mail: [email protected] Website: www.airlifebooks.com Contents Acknowledgements Chronology Foreword 9 Chapter 1 Age of Industrial Development 17 Chapter 2 Days of the Reform Bill 23 Chapters Scheming a Powered Flyer 31 Chapter 4 Publicity Manoeuvring 55 Chapter 5 Trial and Tribulation 63 Chapter 6 Epochal Independent Success 70 Chapter 7 Continuing Development 76 Chapter 8 The Great Exhibition 94 Chapter 9 A Valued Friendship 122 Chapter 10 A Wonderful Old Gentleman 135 Chapter 11 His Son Continues the Quest 154 Chapter 12 An End and a Beginning 168 Index 179 Acknowledgements Introducing some of the many who assisted The route to a biography is long and tortuous and requires the help of many people.