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Aviation Classics Magazine
Avro Vulcan B2 XH558 taxies towards the camera in impressive style with a haze of hot exhaust fumes trailing behind it. Luigino Caliaro Contents 6 Delta delight! 8 Vulcan – the Roman god of fire and destruction! 10 Delta Design 12 Delta Aerodynamics 20 Virtues of the Avro Vulcan 62 Virtues of the Avro Vulcan No.6 Nos.1 and 2 64 RAF Scampton – The Vulcan Years 22 The ‘Baby Vulcans’ 70 Delta over the Ocean 26 The True Delta Ladies 72 Rolling! 32 Fifty years of ’558 74 Inside the Vulcan 40 Virtues of the Avro Vulcan No.3 78 XM594 delivery diary 42 Vulcan display 86 National Cold War Exhibition 49 Virtues of the Avro Vulcan No.4 88 Virtues of the Avro Vulcan No.7 52 Virtues of the Avro Vulcan No.5 90 The Council Skip! 53 Skybolt 94 Vulcan Furnace 54 From wood and fabric to the V-bomber 98 Virtues of the Avro Vulcan No.8 4 aviationclassics.co.uk Left: Avro Vulcan B2 XH558 caught in some atmospheric lighting. Cover: XH558 banked to starboard above the clouds. Both John M Dibbs/Plane Picture Company Editor: Jarrod Cotter [email protected] Publisher: Dan Savage Contributors: Gary R Brown, Rick Coney, Luigino Caliaro, Martyn Chorlton, Juanita Franzi, Howard Heeley, Robert Owen, François Prins, JA ‘Robby’ Robinson, Clive Rowley. Designers: Charlotte Pearson, Justin Blackamore Reprographics: Michael Baumber Production manager: Craig Lamb [email protected] Divisional advertising manager: Tracey Glover-Brown [email protected] Advertising sales executive: Jamie Moulson [email protected] 01507 529465 Magazine sales manager: -
List of Exhibits at IWM Duxford
List of exhibits at IWM Duxford Aircraft Airco/de Havilland DH9 (AS; IWM) de Havilland DH 82A Tiger Moth (Ex; Spectrum Leisure Airspeed Ambassador 2 (EX; DAS) Ltd/Classic Wings) Airspeed AS40 Oxford Mk 1 (AS; IWM) de Havilland DH 82A Tiger Moth (AS; IWM) Avro 683 Lancaster Mk X (AS; IWM) de Havilland DH 100 Vampire TII (BoB; IWM) Avro 698 Vulcan B2 (AS; IWM) Douglas Dakota C-47A (AAM; IWM) Avro Anson Mk 1 (AS; IWM) English Electric Canberra B2 (AS; IWM) Avro Canada CF-100 Mk 4B (AS; IWM) English Electric Lightning Mk I (AS; IWM) Avro Shackleton Mk 3 (EX; IWM) Fairchild A-10A Thunderbolt II ‘Warthog’ (AAM; USAF) Avro York C1 (AS; DAS) Fairchild Bolingbroke IVT (Bristol Blenheim) (A&S; Propshop BAC 167 Strikemaster Mk 80A (CiA; IWM) Ltd/ARC) BAC TSR-2 (AS; IWM) Fairey Firefly Mk I (FA; ARC) BAe Harrier GR3 (AS; IWM) Fairey Gannet ECM6 (AS4) (A&S; IWM) Beech D17S Staggerwing (FA; Patina Ltd/TFC) Fairey Swordfish Mk III (AS; IWM) Bell UH-1H (AAM; IWM) FMA IA-58A Pucará (Pucara) (CiA; IWM) Boeing B-17G Fortress (CiA; IWM) Focke Achgelis Fa-330 (A&S; IWM) Boeing B-17G Fortress Sally B (FA) (Ex; B-17 Preservation General Dynamics F-111E (AAM; USAF Museum) Ltd)* General Dynamics F-111F (cockpit capsule) (AAM; IWM) Boeing B-29A Superfortress (AAM; United States Navy) Gloster Javelin FAW9 (BoB; IWM) Boeing B-52D Stratofortress (AAM; IWM) Gloster Meteor F8 (BoB; IWM) BoeingStearman PT-17 Kaydet (AAM; IWM) Grumman F6F-5 Hellcat (FA; Patina Ltd/TFC) Branson/Lindstrand Balloon Capsule (Virgin Atlantic Flyer Grumman F8F-2P Bearcat (FA; Patina Ltd/TFC) -
Aviation Machinist's Mate 3 & 2
NONRESIDENT TRAINING COURSE Aviation Machinist’s Mate 3 & 2 NAVEDTRA 14008 DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. PREFACE About this course: This is a self-study course. By studying this course, you can improve your professional/military knowledge, as well as prepare for the Navywide advancement-in-rate examination. It contains subject matter about day- to-day occupational knowledge and skill requirements and includes text, tables, and illustrations to help you understand the information. An additional important feature of this course is its reference to useful information in other publications. The well-prepared Sailor will take the time to look up the additional information. History of the course: • Sep 1991: Original edition released. Prepared by ADCS(AW) Terence A. Post. • Jan 2004: Administrative update released. Technical content was not reviewed or revised. Published by NAVAL EDUCATION AND TRAINING PROFESSIONAL DEVELOPMENT AND TECHNOLOGY CENTER TABLE OF CONTENTS CHAPTER PAGE 1. Jet Engine Theory and Design ............................................................................... 1-1 2. Tools and Hardware ............................................................................................... 2-1 3. Aviation Support Equipment.................................................................................. 3-1 4. Jet Aircraft Fuel and Fuel Systems ........................................................................ 4-1 5. Jet Aircraft Engine Lubrication Systems .............................................................. -
Library Additions BOOKS
Library Additions BOOKS GENERAL No12 Squadron during the Lincoln, Bristol Beaufighter, de ‘Sam’ Marshal of the refineries. S J Zaloga. Osprey Low Altitude Bombing System Havilland Mosquito/Vampire/ Royal Air Force The Lord Publishing, Kemp House, (LABS) weapons delivery Venom, English Electric/ Elworthy: a Biography. R Chawley Park, Cumnor Hill, trials among many other BAC Canberra/Strikemaster, Mead. Pen &Sword Aviation, Oxford OX2 9PH, UK. 2019. experiences recalled from a Gloster Meteor, Hawker Pen & Sword Books, 47 96pp. Illustrated. £14.99. ISBN flying career of over 45 years. Hunter/Sea Fury, Hunting Church Street, Barnsley, S 978-14728-3180-4. Percival Jet Provost, Short Yorkshire S70 2AS, UK. 2018. A very detailed analysis of Dorset Aviation Past and Sunderland/Sandringham, xiii; 330pp. Illustrated. £25. the operational effectiveness Present. Royal Aeronautical Supermarine Walrus and ISBN 978-1-52672-717-6. of the USAAF ‘Tidal Wave’ Society Christchurch Branch. SEPECAT Jaguar among A biography of the New mission of 1 August 1943 2016. 50pp. Illustrated. other aircraft types) that were Zealander Air Chief Marshal during WW2 which aimed A concise illustrated either sold to or operated in Sir Charles Elworthy MRAF to destroy strategically history of the development Argentina, Brazil, Chile, Cuba, (1911-1993) – subsequently important oil refineries in of aviation in Bournemouth, Dominican Republic, Ecuador, the Lord Elworthy – who, from Romania using Consolidated Poole, Portland, Weymouth, Mexico, Peru, Uruguay and initially joining the Reserve Air B-24D Liberators flown from Chickerell, Bridport, Toller, Venezuela and the British Force Officers in 1933, rose Benghazi in Libya. Upton, Moreton, Christchurch, colonies of British Guiana/ to being appointed both Chief Global Megatrends Swanage, Weymouth, Belize and the Falklands, of the Air Staff in September German Flak Defences and Aviation: the Warmwell, Tarrant Rushton Bolivia, Guatemala, Honduras, 1963 and also in 1967 Chief vs Allied Heavy Bombers Path To Future-Wise and Hurn. -
RAF Centenary 100 Famous Aircraft Vol 3: Fighters and Bombers of the Cold War
RAF Centenary 100 Famous Aircraft Vol 3: Fighters and Bombers of the Cold War INCLUDING Lightning Canberra Harrier Vulcan www.keypublishing.com RARE IMAGES AND PERIOD CUTAWAYS ISSUE 38 £7.95 AA38_p1.indd 1 29/05/2018 18:15 Your favourite magazine is also available digitally. DOWNLOAD THE APP NOW FOR FREE. FREE APP In app issue £6.99 2 Months £5.99 Annual £29.99 SEARCH: Aviation Archive Read on your iPhone & iPad Android PC & Mac Blackberry kindle fi re Windows 10 SEARCH SEARCH ALSO FLYPAST AEROPLANE FREE APP AVAILABLE FOR FREE APP IN APP ISSUES £3.99 IN APP ISSUES £3.99 DOWNLOAD How it Works. Simply download the Aviation Archive app. Once you have the app, you will be able to download new or back issues for less than newsstand price! Don’t forget to register for your Pocketmags account. This will protect your purchase in the event of a damaged or lost device. It will also allow you to view your purchases on multiple platforms. PC, Mac & iTunes Windows 10 Available on PC, Mac, Blackberry, Windows 10 and kindle fire from Requirements for app: registered iTunes account on Apple iPhone,iPad or iPod Touch. Internet connection required for initial download. Published by Key Publishing Ltd. The entire contents of these titles are © copyright 2018. All rights reserved. App prices subject to change. 321/18 INTRODUCTION 3 RAF Centenary 100 Famous Aircraft Vol 3: Fighters and Bombers of the Cold War cramble! Scramble! The aircraft may change, but the ethos keeping world peace. The threat from the East never entirely dissipated remains the same. -
SP2016-3124855 a Generic Thermodynamic Assessment Of
SP2016-3124855 A Generic Thermodynamic Assessment of Reusable High-Speed Vehicles V. Fernandez Villace, J. Steelant ESA-ESTEC, Section of Aerothermodynamics and Propulsion Analysis Keplerlaan 1, 2200 AG Noordwijk, The Netherlands Email: [email protected], [email protected] ABSTRACT Lifting based vehicles for either space transportation or sustained hypersonic cruise are exposed to high thermal loads during the atmospheric trajectory. The thermal protection system has therefore to efficiently manage the thermal load that penetrates the aeroshell in order to guarantee a satisfactory mission performance. In the present study, the thermal endurance of a LH2-fuelled Mach 8 hypersonic cruiser is assured by soaking the thermal load across the aeroshell into the on-board tank system. The so-produced boil-off acts as a coolant for other aircraft subsystems, like the cabin environmental control system. Further, in order to avoid over-board dumping of the vaporized fuel, a boil-off compression system is proposed to inject the fuel into the propulsion plant. The numerical approach comprised a detailed model of the airframe, where the heat transfer across the interfacing areas between the different subsystems, namely tanks, cabin, propulsion plant and the aeroshell, was resolved based on one-dimensional engineering models. This methodology allowed the evaluation of the complete mission cycle, from the apron, through taxiing and airborne phases and back to apron. 1. INTRODUCTION 2. PRELIMINARY EVALUATION The thermal management of cruising high-speed One of the purposes of the present study was to aircraft plays a very important role. These vehicles design a thermodynamic cycle able to balance the are submitted to high heat loads originating from the airframe thermal and mechanical loads. -
Introduction to Antilock Breaking System (ABS)
Recent Trends in Automation and Automobile Engineering Volume 2 Issue 3 Introduction to Antilock Breaking System (ABS) Sager Sanjay Dawange1*, Vijay P. Satao2 1Sahakar Maharshi Late Bhaskarrao Shigne College, Khamgaon, Buldana, (MS), India 2Siddhivinayak Technical Campus, Shegaon, Buldana, (MS),India. *Corresponding Author E-Mail Id: [email protected] ABSRACT Antilock Braking System (ABS) is very useful in advanced automobiles to avoid slip and lock up of wheel when brakes applied. It is automobile protection system, the regulator is provided to regulate the required torque to sustain optimal slip ration. The slip ration signifies in terms of automobile speed and wheel spin. It is an automated system that relays on principles of threshold braking and cadence braking which were experienced by skilled drivers with former generation braking system. It reaction time is so fast to makes easy steering for the driver. ABS usually deliver advanced vehicle control and reduce the stopping distance in greasy and dry surface, on the other hand on loose surface like pebbles or snow covered pavement, ABS can knowingly rise braking distance, even though still improving vehicle control.[1].The antilock Braking System was developed by Gabriel Voisin in 1929. Keywords: ABS, Antilock breaking system, electrical control unit (ECU) antilock brakes, safety, slip factor, advance braking system, vehicle stability control INTRODUCTION ABS used to be brought in manufacturing Antilock Braking System used to unlock vehicles, such assemblies have develop as the vehicle wheel. An anti-lock braking an increasing number of state-of-the-art system (ABS) is a secure anti-skid braking and active. Modern differences may in gadget that is used on airplane and on land addition no longer only stop wheel lock transport, such as cars, motorcycles, under braking, though it may also alter the trucks, and buses. -
A/C Serial No
A/C SERIAL NO. XW323 SECTION 2B INDIVIDUAL HISTORY BAC JET PROVOST T 5A XW323 /9166M MUSEUM ACCESSION NUMBER 1994/1344/A One of 110 Jet Provost T 5 aircraft ordered under contract no. KC/E/124/CB5(b) dated 29 July 1968; delivered to the RAF from September 1969, including the serial batch XW287 - XW336. 107, including XW323, were later upgraded to T5A standard. Constructor’s number EEP/JP/987? 11 Dec 70 Awaiting collection from British Aircraft Corporation, Warton. Delivered to RAF College Cranwell, Lincs the same day. When new the aircraft was used for the Pilot training of Flt Lt The Prince of Wales - codename ‘Golden Eagle’-at Cranwell as ‘Golden Eagle Two’; he held the rank of Flight Lieutenant. Two Jet Provosts (the other being XW322/1) were held at readiness for use by the Prince during his four-month course; he flew just over 92 hours in Jet Provosts, 23 ½ of them solo on the first Cranwell Graduate Entry course , from 8 March to 20 August 1971. Both had the Royal (Prince of Wales) Cypher on the engine intakes. They were locked under guard in a hangar each night with their own dedicated ground crew. All flights were over a specific airspace over Lincolnshire and monitored by a radar controller based at Northern Radar at RAF Lindholme. Photo of XW322/3 flying together, May 1971 – Royal Flying A Pictorial History Wilson 2017 p.88 Prince Charles joined this first graduate entry at Cranwell, consisting entirely of post-graduates who had already received preliminary pilot training who would receive advanced instruction on Jet Provosts; Instructors were S/Ldr (later CAS) Richard E. -
Conceptual Design for a Supersonic Advanced Military Trainer
Conceptual Design for a Supersonic Advanced Military Trainer A project presented to The Faculty of the Department of Aerospace Engineering San José State University In partial fulfillment of the requirements for the degree Master of Science in Aerospace Engineering by Royd A. Johansen May 2019 approved by Dr. Nikos Mourtos Faculty Advisor © 2019 Royd A. Johansen ALL RIGHTS RESERVED ABSTRACT CONCEPTUAL DESIGN FOR A SUPERSONIC ADVANCED MILITARY TRAINER by Royd A. Johansen The conceptual aircraft design project is based off the T-X program requirements for an advanced military trainer (AMT). The design process focused on a top-level design aspect, that followed the classic aircraft design process developed by J. Roskam’s Airplane Design. The design process covered: configuration selection, weight sizing, performance sizing, fuselage design, wing design, empennage design, landing-gear design, Class I weight and balance, static longitudinal and directional stability, subsonic drag polars, supersonic area rule applied to supersonic drag polars, V-n diagrams, Class II weight and balance, moments and products of inertia, and cost estimation. Throughout the process other materials and references are consulted to verify or develop a better understanding of the concepts in the Airplane Design series. ACKNOWLEDGEMENTS I would like to express my deep gratitude to Dr. Nikos Mourtos for his support throughout this project and his invaluable academic advisement throughout my undergraduate and graduate studies. I would also like to thank Professor Gonzalo Mendoza for introducing Aircraft Design to me as an undergraduate and for providing additional insights throughout my graduate studies. My thanks are also extended to Professor Jeanine Hunter for helping me develop my theoretical foundation in Dynamics, Flight Mechanics, and Aircraft Stability and Control. -
Validation and Parametric Study of Supersonic Air Intake Master’S Thesis in Applied Mechanics
Validation and Parametric Study of Supersonic Air Intake Master's thesis in Applied Mechanics JAKOB EKERMO Department of Mechanics and Maritime Sciences CHALMERS UNIVERSITY OF TECHNOLOGY G¨oteborg, Sweden 2018 MASTER'S THESIS IN APPLIED MECHANICS Validation and Parametric Study of Supersonic Air Intake JAKOB EKERMO Department of Mechanics and Maritime Sciences Division of Fluid Dynamics CHALMERS UNIVERSITY OF TECHNOLOGY G¨oteborg, Sweden 2018 Validation and Parametric Study of Supersonic Air Intake JAKOB EKERMO c JAKOB EKERMO, 2018 Master's thesis 2018:18 Department of Mechanics and Maritime Sciences Division of Fluid Dynamics Chalmers University of Technology SE-412 96 G¨oteborg Sweden Telephone: +46 (0)31-772 1000 Cover: Illustration of complex shock wave patterns residing in the intake for a simulation in the supercritical operating range. Chalmers Reproservice G¨oteborg, Sweden 2018 Validation and Parametric Study of Supersonic Air Intake Master's thesis in Applied Mechanics JAKOB EKERMO Department of Mechanics and Maritime Sciences Division of Fluid Dynamics Chalmers University of Technology Abstract The current study was carried out on behalf of GKN Aerospace as a Master's thesis at Chalmers University of Technology. The Department of Propulsion Engineering at this company wished to develop a deeper understanding into the performance of supersonic engine intakes and to relate this to the influential physical notions and geometry alterations. The ultimate objective was to obtain a CFD model to study the effects of key variations of geometrical and physical parameters on the aerodynamic performance. This model was initially to be validated on a model scale against the results of wind tunnel tests. -
The F-14 Tomcat Story Free
FREE THE F-14 TOMCAT STORY PDF Tony Holmes | 128 pages | 29 Apr 2010 | The History Press Ltd | 9780752449852 | English | Stroud, United Kingdom Tales | F Tomcat You need JavaScript enabled to view it. Everything is welcome about the first flight, the th or th trap, cruise The F-14 Tomcat Story, accident reports, squadron celebrations - whatever you want to go public anonymously with. The birth of the Tomcat logo began in the early '70's by a request from Norm Gandia former No. He asked me to draw. The F Tomcat Association P. Written by Paul Pompier FAs flying vs. Member Login. Remember Me. Featured Products. He asked me to draw Another Tomcat Tale. Written by Jerry "KarateJoe" Watson. The Birth of the Tomcat Logo. Written by Jim Rodriguez. The story of FA, Aircraft No. Written by William Barto. The day I shot myself down. Written by Pete Purvis. My most tense moment in the 26 years of flying Fs. Written by Dale Snodgrass. Crash landing a crippled Tomcat. Written by Anonymous. Written by David Baranek. The F-14 Tomcat Story by the Jolly Rogers. Eject on a familiarization hop. F The F-14 Tomcat Story Air-to-Air Victories. I hope there is a place Written by Paul Pompier. FAs flying vs. German F-4Fs. Written by Hubert Peitzmeier. Written by Bob Norris. The Last of the Jolly. Written by Bob Frantz. Sports Writer Earns The F-14 Tomcat Story Callsign. Written by Rick Reilly. Sunset Glows on the Tomcat. Written by Ward Carroll. Written by Dave Baranek. Zone 5 Afterburner Photo off the Coast of Vietnam. -
NASA Technical Memorandum 85637
NASA Technical Memorandum 85637 NASA-TM-85637 19830020899 HISTORICALDEVELOPMENTOFWORLDWIDE SUPERSONICAIRCRAFT .... _ ;'7"__,'i'_+,'_ .':3 T",,"_r 'r,c'_T_ PO_ "f.........._,,;, 1...,_... _x_..,, M. LeroySpearman MAY 1983 ...iii-i9 _, iQg2 i 'I L_NGLEY RESEARCHCEN rF_k NASA HL_._._TON,VIRGII'_IA National Aeronautics and Space Administration Langley Research Center Hampton,Virginia23665 3 1176 01309 0494 SUMMARY The most dramatic developments in man's quest for increased speed have occurred with the airplane. This paper traces some of the major milestones in the progression of airplane speeds from subsonic to supersonic. While some historical background is included on work done prior to the twentieth century, the major emphasis is on the twentieth century developments after the man-carrying airplane became a practical reality. The techniques of increasing airplane speed revolve around means of increasing the propulsive force and means of reducing the airframe resistance (drag). With the changes in speed, the attendant changes in flow patterns due to the compressibilty of air introduce some aerodynamic problems. In addition, geometric changes introduced to combat the effects of compressibility also promote aerodynamic problems. Someof the solutions to these problems are illustrated, and many inno- vative design features that have evolved are discussed. INTRODUCTION For thousands of years, mankind has been upgrading the methods and means of transportation by land, water, and, finally, air. There has always been a human urge both to move more and to move faster. The progression has included walking; the use of animals; the discovery of the wheel, which, in turn, lead to handcarts, and when combined with animal power, to chariots, wagons, and carriages.