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Raes Annual Report & Accounts 2020
Royal Aeronautical Society Trustees’ Annual Report and Accounts Year Ended 31 December 2020 Charity Registration Number: 313708 Incorporating: Charity Registration Number: 1013530 Charity Registration Number: 1045004 ROYAL AERONAUTICAL SOCIETY REPORT OF THE TRUSTEES FOR YEAR ENDED 31 DECEMBER 2020 Report of the Board of Trustees for the year ended 31 December 2020 The members of the Board of Trustees are pleased to present their annual report and financial statements of the Society for the year ended 31 December 2020. The Trustees confirm that they have complied with the Charities Act 2011 to have due regard to public benefit guidance published by the Charities Commission in determining the activities undertaken by the Society. The financial statements have been prepared in accordance with the accounting polices set out in note 1 to the accounts and comply with the Financial Reporting Standard applicable in the UK and Republic of Ireland (FRS 102) (effective 1 January 2015) - (Charities SORP (FRS 102)). Objectives and Activities Founded in the United Kingdom in 1866, it is the world’s oldest and most respected aeronautical society. The principal objectives of the Society as set out in its Charter of Incorporation granted by letter patent of His Majesty The King George VI in 1949 are “the general advancement of Aeronautical Art, Science and Engineering and more particularly promoting that species of knowledge which distinguishes the profession of Aeronautics.” The Society strives to maintain the highest standards of professionalism in all aerospace disciplines and, as such, the qualifications endowed by the Society are internationally recognised as a professional hallmark. As a learned body, it runs an extensive conference and lecture programme which is available to the public. -
Feeling Supersonic
FlightGlobal.com May 2021 How Max cuts hurt Boeing backlog Making throwaway Feeling aircraft aff ordable p32 Hydrogen switch for Fresson’s Islander p34 supersonic Will Overture be in tune with demand? p52 9 770015 371327 £4.99 Big worries Warning sign We assess A380 Why NOTAM outlook as last burden can delivery looms baffl e pilots 05 p14 p22 Comment Prospects receding Future dreaming Once thought of as the future of air travel, the A380 is already heading into retirement, but aviation is keenly focused on the next big thing Airbus t has been a rapid rise and fall for on who you ask. As we report else- Hydrogen is not without its the Airbus A380, which not so where in this issue, there are those issues, of course, but nonethe- long ago was being hailed as the banking on supersonic speeds be- less it appears more feasible as a future of long-haul air travel. ing the answer. power source for large transport IThe superjumbo would be, The likes of Aerion and Boom Su- aircraft than batteries do at pres- forecasts said, the perfect tool for personic view the ability to shave ent, even allowing for improving airlines operating into mega-hubs significant time from journeys as a energy densities. such as Dubai that were beginning unique selling point. However, there are others who to spring up. While projects are likely to be see hydrogen through a differ- But the planners at Airbus failed technologically feasible, to be able ent filter. They argue that so- to take into consideration the to sell these new aircraft in signif- called sub-regional aircraft – the efficiency gains available from icant volumes their manufacturers Britten-Norman Islander, among a new generation of widebody will have to ensure that supersonic others – can be given fresh impetus twinjets that allowed operators to flight is not merely the domain of if a fuel source can be found that is open up previously uneconomical the ultra-rich. -
The Combat Air Strategy: from Typhoon to 'Tempest'?
BRIEFING PAPER Number 08391, 31 August 2018 The Combat Air Strategy: From Typhoon to By Louisa Brooke-Holland 'Tempest'? What combat aircraft will the RAF be flying in two decades time? The Combat Air Strategy, published in July 2018, sets out the Government’s ambition to develop a new combat air system that will fly alongside Typhoon and Lightning by 2035.1 The aerospace sector accounted for 87% of defence exports over the last ten years and the UK combat air sector has an annual turnover over £6bn.2 The Defence Secretary said the strategy makes clear the UK intends to remain a ‘world leader’ in the combat air sector. Work on the ‘Future Combat Air System Technology Initiative’ has already begun, with Government and industry pledging to invest £2bn over the next decade in exploring new technologies and retaining the skills necessary to develop, design and manufacture a combat aircraft. France and Germany recently announced plans to work together on a future combat air system and the UK will spend the next year talking to a range of potential partners and customers before making some early decisions by the end of 2020 and final investment decisions by 2025. The Strategy announces the creation of a Government/industry partnership called ‘Team Tempest’, drawing on MOD expertise and four major industry partners: BAE Systems, Leonardo, MBDA and Rolls-Royce. Box 1: What is ‘combat air’? “Combat Air refers to aircraft (manned or unmanned) whose prime function is to conduct air-to-air and air- to-surface combat operations in a hostile and contested environment; with the ability to concurrently conduct surveillance, reconnaissance, electronic warfare, and command and control tasks.”3 Tornado, Typhoon, Lightning… Tempest? The RAF’s combat air fleet is about to undergo a massive change. -
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. -
Report by the Senate Rural and Regional Affairs and Transport References Committee
Parliament of the Commonwealth of Australia Air Safety and Cabin Air Quality in the BAe 146 Aircraft Report by the Senate Rural and Regional Affairs and Transport References Committee OCTOBER 2000 ii © Commonwealth of Australia 2000 ISBN 0 642 71093 7 This document was produced from camera-ready copy prepared by the Senate Rural and Regional Affairs and Transport Legislation Committee, and printed by the Senate Printing Unit, Department of the Senate, Parliament House, Canberra. iii MEMBERS OF THE COMMITTEE Members Senator John Woodley AD, Queensland Chairman Senator Winston Crane LP, Western Australia Deputy Chairman Senator Jeannie Ferris LIB, South Australia Senator Michael Forshaw ALP, New South Wales Senator Sue Mackay ALP, Tasmania Senator Kerry O’Brien ALP, Tasmania Participating Members Senator Abetz Senator Faulkner Senator McLucas Senator Bartlett Senator Ferguson Senator Mason Senator Boswell Senator Gibson Senator S Macdonald Senator Brown Senator Harradine Senator Murphy Senator Buckland Senator Harris Senator Payne Senator Calvert Senator Hutchins Senator Tchen Senator Chapman Senator Knowles Senator Tierney Senator Coonan Senator Lightfoot Senator Watson Senator Crossin Senator McGauran Senator West Senator Eggleston Senator McKiernan Committee Secretariat The Senate Parliament House Canberra ACT 2600 Telephone (02) 6277 3511 Facsimile (02) 6277 5811 Internet www.aph.gov.au/senate Email [email protected] TABLE OF CONTENTS MEMBERS OF THE COMMITTEE ............................................................. iii TABLE -
REVIEW of PROPULSION-INDUCED EFFECTS on AERODYNAMICS of JET/STOL AIRCRAFT by Richnrd J
NASA TECHNICAL NOTE REVIEW OF PROPULSION-INDUCED EFFECTS ON AERODYNAMICS OF JET/STOL AIRCRAFT by Richnrd J. Margason Langley Research Center Langley Station, Hampton, Vae NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON, D. C. FEBRUARY 1970 TECH LIBRARY WFB, NM 1. Report No. 2. Government Accession No. 3. Recipient’s Catalog No. NASA TN D-5617 I I 5. Report Date 4. Title and Subtitle REVIEW OF PROPULSION-INDUCED EFFECTS ON AERODYNAMICS OF I February 1970 JET V/STOL AIRCRAFT 6. Performing Orgonization Code 7. Authods) 8. Performing Orgoni Lotion Report Richard J. Margason I L-6565 (10. Work Unit No. 721-01- 11-05-23 9. Performing Orgonizotion Name ond Address 11. Contract or Grant No. NASA Langley Research Center - I Hampton, Va. 23365 13. Type of Report and Period Cov, 12. Sponsoring Agency Name and Address Technical Note National Aeronautics and Space Administration Washington, D.C. 20546 14. Sponsoring Agency Code 15. Supplementory Notes This material was originally presented as a lecture at the University of Tennessee Space Institute Short Course on V/STOL, November 1968. 16. Abstract This paper reviews several aspects of the effects induced on the aerodynamics of V/STOL aircraft in hover and transition flight by the interference of wakes from relatively high disk-loading propulsion devices. Four problem areas are treated: (1) the performance losses sustained when hovering out of ground effect, (2) induced aerodynamic effects in transition flight out of ground effect, (3) the problems caused by hot-gas ingestion, and (4) the effects induced on performance during hover in ground effect. Some of the conflicts among the design requirements imposed by these different modes of flight are discussed, along with the present state of the art of solutions to some of the problems. -
The Expected Wave-Off by Richard Carlson SSF Chairman
The Expected Wave-Off by Richard Carlson SSF Chairman The February morning was bright and clear, just as the forecast had predicted. It was a perfect day to go out to the glider school and knock some rust off and beat those Chicago winter blues. With the forecast for temperatures in the low 40’s and no snow on the grass runway, a group of us made arrangements to meet Saturday morning for some winter flying. Nobody expected thermals, and we were not disappointed flying only sled rides in our trusty Blanik L-13. We all pitched in to ready the glider for flight, doing the pre-flight inspection and securing the rear seat belts as everyone was going solo to get current. Today our Green Citrabria would be doing the towing duties. It was pre-heated, started and test flown, all systems go. My turn finally arrived and I eagerly climbed into the front seat, buckled up , ran the flow, and conducted the checklist. The lack of an electrical system meant no radio or audio vario, just basic analog gauges for Airspeed, Altitude, and Vario - Check. Belts on and adjusted, rear seat belts fastened to avoid any fouling of the controls - Check. No ballast installed and none required – Check. Flaps and Dive brakes closed and handles in the lock detent, stick and rudder pedals free travel in all directions, trim set for take-off – Check. Towplane in position, no knots in the rope, proper towring attached and verified – Check. Canopy close and locked, vents open to keep it from fogging over – Check. -
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. -
SPRUE EXAMINER Engine Pods and Tailfins
Vol. 16, No.11 Newsletter of the Austin Scale Modelers Society November 2008 have after I had it put together. There is a Building the Mobius Seaview lighting kit available from VoodooFx by (www.voodoofx.com) for $60.00, but I had my Bill Delk, IPMS #35227 own ideas on what I wanted to see in my mind. Besides, I think I spent under $20.00 for my Make no mistake; this is a large model, parts. measuring almost 39 inches from nose to tail. The scale is approximately 1/128th. The total I followed the painting instructions for the kit parts count is 110 light gray and 19 clear styrene to paint all the parts in the control room before parts. That includes the 4-part stand, Flying assembly. Part of the control room wall on the Sub, Mini Sub, and Diving Bell. The four-page port side of the sub (left side facing the bow instruction is in black and white with four looking from the rear of the sub for all us diagrams and descriptive text, eight-page history landlubber types) was a bank of blinking lights of the Seaview, plus an one-page painting color simulating the ship's computer. I wanted to try chart. There are already several aftermarket and simulate this effect. I built the electronic resin, photoetch and decal kits available for this circuit with ten blinking LEDs and drilled out model, but I chose not to purchase them. many of the indentations that simulated the lighting. It looked great when you could look at If you are not fond of sanding and seam filling, it straight on. -
Records Fall at Farnborough As Sales Pass $135 Billion
ISSN 1718-7966 JULY 21, 2014 / VOL. 448 WEEKLY AVIATION HEADLINES Read by thousands of aviation professionals and technical decision-makers every week www.avitrader.com WORLD NEWS More Malaysia Airlines grief The Airbus A350 XWB The US stock market fell sharply was a guest on fears of renewed hostilities of honour at after the news that a Malaysian Farnborough Airlines flight was allegedly shot (left) last week down over eastern Ukraine, with as it nears its service all 298 people on board reported entry date dead. US vice president Joe Biden with Qatar said the plane was “blown out of Airways later the sky”, apparently by a surface- this year. to-air missile as the Boeing 777 Airbus jet cruised at 33,000 feet, some 1,000 feet above a closed section of airspace. Ukraine has accused Records fall at Farnborough as sales pass $135 billion pro-Russian “terrorists” of shoot- Airbus, CFM International beat forecasts with new highs at UK show ing the plane down with a Soviet- era SA-11 missile as it flew from The 2014 Farnborough Interna- Farnborough International Airshow: Major orders* tional Airshow closed its doors Amsterdam to Kuala Lumpur. Airframer Customer Order Value¹ last week safe in the knowledge Boeing 777 Qatar Airways 50 777-9X $19bn Record show for CFM Int’l that it had broken records on many fronts - not least on total Boeing 777, 737 Air Lease 6 777-300ER, 20 737 MAX $3.9bn CFM International, the 50/50 orders and commitments for Air- Airbus A320 family SMBC 110 A320neo, 5 A320 ceo $11.8bn joint company between Snec- bus and Boeing aircraft, which ma (Safran) and GE, celebrated Airbus A320 family Air Lease 60 A321neo $7.23bn hit a combined $115.5bn at list record sales worth some $21.4bn Embraer E-Jet Trans States 50 E175 E2 $2.4bn prices for 697 aircraft - over 60% at Farnborough. -
20150014387.Pdf
General Disclaimer One or more of the Following Statements may affect this Document • This document has been reproduced from the best copy furnished by the organizational source. It is being released in the interest of making available as much information as possible. • This document may contain data, which exceeds the sheet parameters. It was furnished in this condition by the organizational source and is the best copy available. • This document may contain tone-on-tone or color graphs, charts and/or pictures, which have been reproduced in black and white. • This document is paginated as submitted by the original source. • Portions of this document are not fully legible due to the historical nature of some of the material. However, it is the best reproduction available from the original submission. Produced by the NASA Center for Aerospace Information (CASI) MR No. I.6F25 . 1' I FILE NJ.TIO AL ADVIS' c~e FYAEBJJNAUTICS • I DBE AODR ED MEMORANDUY REPORT f ~. S1 'i; T, . ·, FO AE O Aur, ~~r'N1£"lt"1'2S;,-' D', • 'hA for the 1 J lo Qf.;t~Ol '.) \ ec \o H' ~ e 'J Ctars if,(" t> Air Materiel Command, Army Air Forces 0 ~ Le,._ \2.(, r e,uvikl TF.STS OF A 1/S-SCALE MODEL OF THE REPUBLIC . ~ Le..\-W c~u J . XP-84 AIRPLANE (ARMY PROJECT MX-$78) IN THE (sco 0 /\cl \C()~{ ~ 'f"u/\.L I~ > .... r u... '1 rro~ -r , v" u LAWLEY 300 MPH 7- BY 10-Foor TUNNEL S:. n By Warren A.. Tucker a:rxi Kenneth W. -
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.