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Cross & Cockade International SERIALS with PHOTOGRAPHS
Cross & Cockade International THE FIRST WORLD WAR AVIATION HISTORICAL SOCIETY Registered Charity No 1117741 www.crossandcockade.com INDEX for SERIALS with PHOTOGRAPHS This is a provisional index of all the photographs of aircraft with serial numbers in the 46 years of the Cross & Cockade Journal. There are only photographs with identifiable serials, no other items are indexed. Following the Aircraft serial number is the make & model in parentheses, then page number format is: first the volume number, followed by the issue number (1 to 4) between periods with the page number(s) at the end. The cover pages use the last three characters with a 'c' (cover) 'f' - 'r'(front-rear), '1'(outside) '2' (inside). There are over 4180 entries in three categories, British individual aircraft, other countries individual aircraft, followed by airships & balloons. Regretfully, copies of the photographs are not available. Derek Riley, Jan. 22, 2017 AIRCRAFT SERIAL, BRITISH INDIVIDUAL...............................pg 01 AIRCRAFT SERIALS, OTHER COUNTRY...................................pg 13 AIRSHIPS & BALLOONS.............................................................pg 18 AIRCRAFT SERIAL, British individual 81 (Short Folder Seaplane) 07.1.024, 184 (Short Admiralty Type 184) 04.1.cr2, Serial Aircraft type Page num 07.1.027, 15.4.162 06.4.152, 06.4.cf1, 15.4.166, 16.2.064 2 (Short Biplane) 15.4.148 88 (Borel Seaplane) 15.4.167, 16.2.056 187 (Wight Twin Seaplane) 16.2.065 9 (Etrich Taube Monoplane) 15.4.149, 95 (M.Farman Seaplane) 03.4.139, 16.2.057 201 (RAF BE1) 08.4.150, 36.4.256, 42.3.149 46.4.266 97 (H.Farman Biplane) 16.2.057 202 (Bréguet L.2 biplane) 08.4.149 10 (Short Improved S41 Type) 23.4.171, 98 (H.Farman Biplane) 15.4.157 203 (RAF BE3) 08.4.152, 09.4.172, 20.3.134, 34.1.065 103 (Sopwith Tractor Biplane) 15.4.157, 20.3.135, 23.4.169, 28.4.182, 38.4.239, 14 (Bristol Coanda monoplane) 45.3.176 15.4.165 38.4.242, 41.3.162 16 (Avro 503) 15.4.150 104 (Sopwith Tractor Biplane) 03.4.143 204 (RAF BE4) 20.3.134, 23.4.176, 36.1.058 17 (Hydro Recon. -
Airwork Limited
AN APPRECIATION The Council of the Royal Aeronautical Society wish to thank those Companies who, by their generous co-operation, have done so much to help in the production of the Journal ACCLES & POLLOCK LIMITED AIRWORK LIMITED _5£ f» g AIRWORK LIMITED AEROPLANE & MOTOR ALUMINIUM ALVIS LIMITED CASTINGS LTD. ALUMINIUM CASTINGS ^-^rr AIRCRAFT MATERIALS LIMITED ARMSTRONG SIDDELEY MOTORS LTD. STRUCTURAL MATERIALS ARMSTRONG SIDDELEY and COMPONENTS AIRSPEED LIMITED SIR W. G. ARMSTRONG WHITWORTH AIRCRAFT LTD. SIR W. G. ARMSTRONG WHITWORTH AIRCRAFT LIMITED AUSTER AIRCRAFT LIMITED BLACKBURN AIRCRAFT LTD. ^%N AUSTER Blackburn I AIRCRAFT I AUTOMOTIVE PRODUCTS COMPANY LTD. JAMES BOOTH & COMPANY LTD. (H1GH PRECISION! HYDRAULICS a;) I DURALUMIN LJOC kneed *(6>S'f*ir> tttaot • AVIMO LIMITED BOULTON PAUL AIRCRAFT L"TD. OPTICAL - MECHANICAL - ELECTRICAL INSTRUMENTS AERONAUTICAL EQUIPMENT BAKELITE LIMITED BRAKE LININGS LIMITED BAKELITE d> PLASTICS KEGD. TEAM MARKS ilMilNIICI1TIIH I BRAKE AND CLUTCH LININGS T. M. BIRKETT & SONS LTD. THE BRISTOL AEROPLANE CO., LTD. NON-FERROUS CASTINGS AND MACHINED PARTS HANLEY - - STAFFS THE BRITISH ALUMINIUM CO., LTD. BRITISH WIRE PRODUCTS LTD. THE BRITISH AVIATION INSURANCE CO. LTD. BROOM & WADE LTD. iy:i:M.mnr*jy BRITISH AVIATION SERVICES LTD. BRITISH INSULATED CALLENDER'S CABLES LTD. BROWN BROTHERS (AIRCRAFT) LTD. SMS^MMM BRITISH OVERSEAS AIRWAYS CORPORATION BUTLERS LIMITED AUTOMOBILE, AIRCRAFT AND MARITIME LAMPS BOM SEARCHLICHTS AND MOTOR ACCESSORIES BRITISH THOMSON-HOUSTON CO., THE CHLORIDE ELECTRICAL STORAGE CO. LTD. LIMITED (THE) Hxtie AIRCRAFT BATTERIES! Magnetos and Electrical Equipment COOPER & CO. (B'HAM) LTD. DUNFORD & ELLIOTT (SHEFFIELD) LTD. COOPERS I IDBSHU l Bala i IIIIKTI A. C. COSSOR LIMITED DUNLOP RUBBER CO., LTD. -
CEAS Quarterly Bulletin Talented Engineers Are Needed
The Quarterly Bulletin of the COUNCIL OF EUROPEAN AEROSPACE SOCIETIES 3AF– AIAE– AIDAA– DGLR– FSAE– FTF– HAES– NVvL– RAeS– SVFW–TsAGI • GENERAL • AERONAUTICS • SPACE • Issue 2 – 2009 • June • Editorial INVESTING IN YOUTH The future of Europe is in the hands of its youth: this is a basic truth. However, surprisingly, while we are full in course of the election campaign for the renewal of the European Parliament, we hear almost nothing about education and culture, and we see no proposals from the candidates on how to prepare the students and young professionals to live in an increasingly integrated Europe. The question is a very broad and difficult one, due to the large number of Member States and the diversity of languages and cultures; but this is all the more reason to concentrate great efforts on it. In the aerospace sector, the projects, more and more complex, are developed across several national borders and include the highest technologies. So, to overcome the Jean-Pierre Sanfourche numerous challenges which confront us in a fierce world-wide aerospace market, Editor-in-Chief, CEAS Quarterly Bulletin talented engineers are needed. Unfortunately, in the past two or three decades within Europe, there have been clear indications that the most brilliant students pre- fer careers in business and finance to those in science, technology and engineering. Action is clearly necessary to reverse this trend by taking the measures that will CONTENTS allow us to attract and then retain the best talent in the air and space activities. The GENERAL Pages organising Committee of the upcoming CEAS2009 Air & Space Conference in Manchester has taken an important step in this direction by including in the • The ASD President’s message 2 Conference agenda the launch of a new European Young Aerospace Professional • The life of the CEAS 4 (EYAP) forum. -
2021-03 Pearcey Newby and the Vulcan V2.Pdf
Journal of Aeronautical History Paper 2021/03 Pearcey, Newby, and the Vulcan S C Liddle Vulcan to the Sky Trust ABSTRACT In 1955 flight testing of the prototype Avro Vulcan showed that the aircraft’s buffet boundary was unacceptably close to the design cruise condition. The Vulcan’s status as one of the two definitive carrier aircraft for Britain’s independent nuclear deterrent meant that a strong connection existed between the manufacturer and appropriate governmental research institutions, in this case the Royal Aircraft Establishment (RAE) and the National Physical Laboratory (NPL). A solution was rapidly implemented using an extended and drooped wing leading edge, designed and high-speed wind-tunnel tested by K W Newby of RAE, subsequently being fitted to the scaled test version of the Vulcan, the Avro 707A. Newby’s aerodynamic solution exploited a leading edge supersonic-expansion, isentropic compression* effect that was being investigated at the time by researchers at NPL, including H H Pearcey. The latter would come to be associated with this ‘peaky’ pressure distribution and would later credit the Vulcan implementation as a key validation of the concept, which would soon after be used to improve the cruise efficiency of early British jet transports such as the Trident, VC10, and BAC 1-11. In turn, these concepts were exploited further in the Hawker-Siddeley design for the A300B, ultimately the basis of Britain’s status as the centre of excellence for wing design in Airbus. Abbreviations BS Bristol Siddeley L Lift D Drag M Mach number CL Lift Coefficient NPL National Physical Laboratory Cp Pressure coefficient RAE Royal Aircraft Establishment Cp.te Pressure coefficient at trailing edge RAF Royal Air Force c Chord Re Reynolds number G Load factor t Thickness HS Hawker Siddeley WT Wind tunnel HP Handley Page α Angle of Attack When the airflow past an aerofoil accelerates its pressure and temperature drop, and vice versa. -
Aircraft Engines and Strategic Bombing in the First World War
Aircraft Engines and Strategic Bombing in the First World War Todd Martin Published: 27 January 2016 Contents Historiography, Acknowledgments and Introduction . .3 Table I: Comparative Aircraft Engines . .5 Table II: Aircraft Engine Production, 1914-1918 . .5 Map: British Independent Force Squadron No. 55 DH-4 Day Bombing Raids, Germany, 1918 . .6 Abbreviations . .7 Part I: Aircraft Engines 1. Austria and Germany . .8 2. France . .17 3. United States . .23 4. Britain . .29 Part II: Strategic Bombing 5. The Channel . .37 6. The Rhine . .46 7. Amanty . .53 Conclusion . .69 Bibliography . .70 Title Page: NARA, RG 120, M990/10, B VII 124, Statistical Analysis of Aerial Bombardments, Report No. 110, Statistics Branch - General Staff, War Department, Nov. 7, 1918. 2 Historiography, Acknowledgements and Introduction Historiography and Acknowledgments arithmetic however which makes the following a revi- The following avoids repeating much of the well sion of the thesis of Irving B. Holley, Jr.’s Ideas and known stories of the Liberty aircraft engine and the Weapons (1953) that the American military aviation controversies surrounding American aviation in the effort in the First World War failed due to a lack of First World War. It also avoids offering a definition of airpower doctrine, a revision the need for which is strategic bombing, save to suggest that economic war- pointed to in the second volume of Mauer Mauer’s fare may be properly considered to be an element of edition of The U.S. Air Service in World War I (1978.) that definition. The following adheres to the long The continuing efforts to understand the world established understanding that many of the aircraft wars as a single historical event and to study them engines successfully used during that war were “from the middle” perspective of technology and derived from an engine designed before the war by engineering1 are appropriate and admirable and thus Ferdinand Porsche. -
PRESS RELEASE Safran: Continued Momentum in Q3 2019
PRESS RELEASE Safran: Continued momentum in Q3 2019 On track to meet 2019 outlook Paris, October 31, 2019 Adjusted data Q3 2019 revenue at Euro 6,095 million, up 14.0% on a reported basis and up 9.8% on an organic basis 9M 2019 revenue at Euro 18,197 million, up 22.5% on a reported basis and up 12.6% on an organic basis 2019 outlook confirmed Consolidated data Consolidated revenue was Euro 6,180 million in Q3 2019 Consolidated revenue was Euro 18,495 million for 9M 2019 Foreword . All figures in this press release represent adjusted [1] data, except where noted. Please refer to the definitions and reconciliation between Q3 2019 and 9M 2019 consolidated revenue and adjusted revenue. Please refer to the definitions contained in the Notes on page 8 of this press statement; . Aerosystems and Aircraft Interiors (former Zodiac Aerospace activities) are fully consolidated in Safran’s financial statements from March 1, 2018; . Organic variations exclude changes in scope (notably the contribution of Aerosystems and Aircraft Interiors in January and February 2019) and currency impacts for the period; . Safran disclosed a new presentation of segment information as of June 30, 2019 (see press release of July 1, 2019); . The 2019 outlook was prepared taking into consideration the full application of IFRS16. Executive commentary CEO Philippe Petitcolin commented: “In the third quarter, we took another step towards meeting our 2019 organic growth revenue target. The 9.8% organic growth is strong considering the comparison basis and in line with year-end outlook. Regarding the MAX grounding, we are supporting Boeing and based on our current production rate of LEAP-1B engines corresponding to 42 aircraft a month, we confirm a production of around 1 800 LEAP engines in 2019.” 1 WorldReginfo - 49595b9c-6546-491f-b69b-1ac6c9717381 Key business highlights 1- Aerospace Propulsion Continuing growth of narrowbody engine deliveries At the end of September 2019, combined shipments of CFM56 and LEAP engines reached 1,643 units, compared with 1,575 in 2018. -
The CFM Engine Saga
The CFM Engine Saga Jean-Paul Ebanga, CFM President Aircraft Builder Council Conference, San Diego September 23, 2013 CFM, CFM56, LEAP and the CFM logo are trademarks of CFM International, a 50/50 joint company between Snecma (Safran group) and GE. The information in this document is CFM Proprietary Information and is disclosed in confidence. It is the property of CFM International and its parent companies, and shall not be used, disclosed to others or reproduced without the express written consent of CFM. If consent is given for reproduction in whole or in part, this notice shall appear in any such reproduction in whole or in part. The information contained in this document may also be controlled by the U.S. and French export control laws. Unauthorized export or re-export is prohibited. 1923 Fokker T2 2 / CFM Proprietary Information subject to restrictions on the cover What is CFM? 3 / CFM Proprietary Information subject to restrictions on the cover CFM is a JV … Most successful World’s largest aircraft Most successful aviation venture engine company aviation partnership • 25000+ engines shipped • 70% share/100+ PAX GE – Safran Agreement • 18K to 50K lbs. thrust • Together since 1974 • Committed until 2040 4 / CFM Proprietary Information subject to restrictions on the cover with a perfect solution line-up … 5 / CFM Proprietary Information subject to restrictions on the cover … using a very lean organization * All activities shared 50/50: R&D, CFM56 and LEAP, a same worksharing engineering, sales and marketing, product support, manufacturing -
Quick Install Guide
QIG 253271827A Fast 1704_GB without WPS.book Page 1 Mercredi, 7. octobre 2009 2:47 14 SAGEM F@st™ 1704 Quick Installation Guide QIG 253271827A Fast 1704_GB without WPS.book Page 1 Mercredi, 7. octobre 2009 2:47 14 SAGEM F@stTM 1704 Sagem Communications SAS (hereafter referred to as Sagem Communications) thanks you for choosing the range of SAGEM F@stTM 1704 routers while hoping that it will provide you with full satisfaction. SAGEM F@stTM 1704 products adapt the ADSL function respectively on POTS (ITU G.992.1/3/5 - Appendix A) and on ISDN (ITU G.992.1/3/5 - Appendix B). SAGEM F@stTM 1704 equipment include four ethernet interfaces (LAN1 to LAN4). In addition, this router will provide you with access to all the services provided by your Internet Access Provider, as shown in the diagram below. CE marking: The CE marking certifies that the product complies with the essential requirements of the Directive 1999/5/EC concerning radio equipment and telecommunication equipment, and of Directives 2006/95/EC concerning safety and 2004/108/EC concerning electromagnetic compatibility, defined by the European Parliament and Council to reduce electromagnetic interferences and protect the health and safety of users. The product named SAGEM F@stTM 1704 can be operated in the European Union without restrictions indoor but cannot be operated in France in the whole of the band until further notice. The CE declaration of conformity can be viewed in the support section of the Sagem Communications site www.sagem-communications.com, or it can be obtained from the following address: Sagem Communications SAS - Customer relations department 250, Route de l'Empereur 92500 RUEIL MALMAISON - FRANCE Copyright © Sagem Communications SAS All rights reserved. -
Safranin 2013
SAFRAN IN 2013 2013 REGISTRATION DOCUMENT WorldReginfo - ad8c403d-4ac5-44b4-b8b3-bd5c47afcfb7 SAFR_1402217_RA_2013_GB_CouvDocRef.indd 1 26/03/14 12:12 Contents GROUP PROFILE 1 1 PRESENTATION OF THE GROUP 8 5.3 Developing human potential 203 5.4 Aiming for excellence in health, 1.1 Overview 10 safety and environment 214 1.2 Group strategy 14 5.5 Involving our suppliers and partners 224 1.3 Group businesses 15 5.6 Investing through foundations 1.4 Competitive position 32 and corporate sponsorship 224 1.5 Research and development 32 5.7 CSR reporting methodology and Statutory 1.6 industrial investments 37 Auditors’ report 226 1.7 Sites and production plants 38 1.8 Safran Group purchasing strategy 43 6 CORPORATE GOVERNANCE 232 1.9 Safran quality performance and policy 43 6.1 Board of Directors and Executive 1.10 Safran+ progress initiative 44 Management 234 6.2 Executive Corporate Officer 2 REVIEW OF OPERATIONS IN 2013 compensation 263 AND OUTLOOK FOR 2014 46 6.3 Share transactions performed by Corporate Officers and other managers 272 2.1 Comments on the Group’s performance 6.4 Audit fees 274 in 2013 based on adjusted data 48 6.5 Report of the Chairman 2.2 Comments on the consolidated of the Board of Directors 276 financial statements 66 6.6 Statutory Auditors’ report 2.3 Comments on the parent company on the report prepared by the Chairman financial statements 69 of the Board of Directors 290 2.4 Outlook for 2014 71 2.5 Subsequent events 71 7 INFORMATION ABOUT THE COMPANY, 3 THE CAPITAL AND SHARE FINANCIAL STATEMENTS 72 OWNERSHIP 292 3.1 -
The Connection
The Connection ROYAL AIR FORCE HISTORICAL SOCIETY 2 The opinions expressed in this publication are those of the contributors concerned and are not necessarily those held by the Royal Air Force Historical Society. Copyright 2011: Royal Air Force Historical Society First published in the UK in 2011 by the Royal Air Force Historical Society 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. ISBN 978-0-,010120-2-1 Printed by 3indrush 4roup 3indrush House Avenue Two Station 5ane 3itney O72. 273 1 ROYAL AIR FORCE HISTORICAL SOCIETY President 8arshal of the Royal Air Force Sir 8ichael Beetham 4CB CBE DFC AFC Vice-President Air 8arshal Sir Frederick Sowrey KCB CBE AFC Committee Chairman Air Vice-8arshal N B Baldwin CB CBE FRAeS Vice-Chairman 4roup Captain J D Heron OBE Secretary 4roup Captain K J Dearman 8embership Secretary Dr Jack Dunham PhD CPsychol A8RAeS Treasurer J Boyes TD CA 8embers Air Commodore 4 R Pitchfork 8BE BA FRAes 3ing Commander C Cummings *J S Cox Esq BA 8A *AV8 P Dye OBE BSc(Eng) CEng AC4I 8RAeS *4roup Captain A J Byford 8A 8A RAF *3ing Commander C Hunter 88DS RAF Editor A Publications 3ing Commander C 4 Jefford 8BE BA 8anager *Ex Officio 2 CONTENTS THE BE4INNIN4 B THE 3HITE FA8I5C by Sir 4eorge 10 3hite BEFORE AND DURIN4 THE FIRST 3OR5D 3AR by Prof 1D Duncan 4reenman THE BRISTO5 F5CIN4 SCHOO5S by Bill 8organ 2, BRISTO5ES -
Sagem Axiumtm Hd-D56b Tm High-Definition Dlp Screen, 142 Cm - 16/9
SAGEM AXIUMTM HD-D56B TM HIGH-DEFINITION DLP SCREEN, 142 CM - 16/9 > INDULGE IN EXTRA-WIDE IMAGES > HOME CINEMA DESIGN > FULL CONNECTIVITY • Piano black edging Ability to create a professional, • Timeless design multimedia and entertainment arena • Compact stand • Capability for up to 8 TV peripherals to be simultaneously connected • 142 cm diagonal screen • 8 video inputs, 2 PC inputs • 44 cm in depth "1 digital DVI with HDCP control and 1 analogue VGA" • All-in-one table-top style with a matching stand unit • Automatic input/output detection (available as an optional extra) > A VISIBLY BIGGER TECHNOLOGY > AN OPTIMUM PICTURE QUALITY TM DLP , the most innovative technology of today bringing Enjoy a picture of exceptional quality, advanced features precision and brightness TM DLP technology 2 • • Spectacular brightness: 700 cd/m • PIP function, PAP, PAT, Teletext and Electronic Programme Guide (EPG) • Unrivalled contrast: 3000:1 • Double tuner • Ultra-high resolution picture with up to 1 million pixels (1280 x 720), • Picture: 5 setting modes, 8 types of format TM and extremely rich colours, DCDi image processing by FAROUDJA, anti-reflection coating and high viewing angle • DMD: HD2+ providing a picture with greater contrast and detail > READY FOR HIGH-DEFINITION TELEVISION • 720-line display in progressive mode (720p) and 1080-line display in > AN ADAPTABLE SOUND SYSTEM interlaced mode (1080i) • Ready to read visual content in High-Definition for quality up to 20 times Adapt the sound to your requirements superior than that of electro-magnetic TV and up to 3 times better than DVD • Integrated Nicam stereo audio sound • Smart sound volume control • Sound graphic equalizer • 2 loud side-speaker outputs SAGEM AXIUMTM, A VISIONARY LEAD SAGEM AXIUMTM HD-D56B: HIGH-DEFINITION DLPTM SCREEN, 142 CM - 16/9 > INDULGE IN EXTRA-WIDE IMAGES A. -
Handley Page, Lachmann, Flow Control and Future Civil Aircraft
Handley Page, Lachmann, flow control and future civil aircraft John Green ABSTRACT Frederick Handley Page and Gustav Lachmann independently developed and patented the concept of the slotted wing as a means of increasing maximum lift. Subsequently they co-operated on the project and Lachmann joined Handley Page Ltd. The Handley Page slotted wing became used worldwide, generating substantial income for the company from use of the patent, and its descendents can be found on all modern transport aircraft. In the years following World War II, Lachmann led research at Handley Page to reduce drag by keeping the boundary layer laminar by surface suction. Handley Page led this field in the UK and developed a number of aircraft concepts, none of which came to fruition as full scale projects. However, looking to the future, the basic concept of laminar flow control holds out arguably the greatest potential of all technologies for reducing the fuel burn and environmental impact of future civil aircraft. 1. INTRODUCTION This is the story of two men of genius, Frederick Handley Page and Gustav Lachmann, Figs. 1 and 2. They were brought together by chance, as a result of having independently, and unknown to each other, invented and patented the same aerodynamic concept. During World War I they had been on opposite sides. Handley Page, who had been 28 at the outbreak of hostilities, established his company’s reputation as the designer of the large biplane bombers, the ‘bloody paralysers’ sought by the Royal Navy in 1914, that made a great contribution to the war effort in 1917 and 1918.