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The Bloodhound Guided Missile and the Hawker Harrier “Jump Jet”
Draft for joint Herbert Simon Institute/Manchester Institute of Innovation Research Seminar, 1st April 2011 Practice in Communities: how engineers create solutions ‐ the Bloodhound Guided Missile and the Hawker Harrier “jump jet”. Jonathan Aylen* and Mike Pryce* Manchester Institute of Innovation Research Manchester Business School University of Manchester “Every aeroplane is different ‐ a self‐optimising shambles” Ralph Hooper, Harrier project designer Aerospace engineers face the task of developing a project from overall design concept through to working prototype and on into sustained use. Engineers often work in small groups when developing an initial concept. Once the basic concept has been agreed they may work in similarly small groups, or as part of larger teams to develop key components of a system. At this stage key design tasks are defined and delegated and then the resulting components are tested and integrated to build a prototype (Vincenti, 1990). Individual sub‐assemblies are usually developed in parallel. So, aeronautical engineering is often seen as a cyclical process of analysis and synthesis, although in practice it is seldom so neat and linear, as the opening quote from a leading practitioner, Ralph Hooper, illustrates. The nature of engineering design is complex, with designers having to cope with many systems and components interacting in dynamic ways. The breadth and depth of knowledge required means no one person can carry out all the tasks of engineering design. Group or team working is essential. Engineering design is an innately social activity. However, mastering the specific skills of any one discipline, and also learning how to utilise the knowledge gained within the group or team, often depends on the abilities of key individuals. -
Turbulence in the Gulf
Come and see us at the Dubai Airshow on Stand 2018 AEROSPACE November 2017 FLYING FOR THE DARK SIDE IS MARS GETTING ANY CLOSER? HYBRID-ELECTRIC PROPULSION www.aerosociety.com November 2017 Volume 44 Number 11 Volume TURBULENCE IN THE GULF SUPERCONNECTOR AIRLINES BATTLE HEADWINDS Royal Aeronautical Society Royal Aeronautical N EC Volume 44 Number 11 November 2017 Turbulence in Is Mars getting any 14 the Gulf closer? How local politics Sarah Cruddas and longer-range assesses the latest aircraft may 18 push for a human impact Middle mission to the Red East carriers. Planet. Are we any Contents Clément Alloing Martin Lockheed nearer today? Correspondence on all aerospace matters is welcome at: The Editor, AEROSPACE, No.4 Hamilton Place, London W1J 7BQ, UK [email protected] Comment Regulars 4 Radome 12 Transmission The latest aviation and Your letters, emails, tweets aeronautical intelligence, and feedback. analysis and comment. 58 The Last Word Short-circuiting electric flight 10 Antenna Keith Hayward considers the Howard Wheeldon looks at the current export tariff spat over MoD’s planned Air Support to the Bombardier CSeries. Can a UK low-cost airline and a US start-up bring electric, green airline travel Defence Operational Training into service in the next decade? On 27 September easyJet revealed it had (ASDOT) programme. partnered with Wright Electric to help develop a short-haul all-electric airliner – with the goal of bringing it into service within ten years. If realised, this would represent a game-changing leap for aviation and a huge victory for aerospace Features Cobham in meeting or even exceeding its sustainable goals. -
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) -
Pegasus Vectored-Thrust Turbofan Engine
Pegasus Vectored-thrust Turbofan Engine Matador Harrier Sea Harrier AV-8A International Historic Mechanical Engineering Landmark 24 July 1993 International Air Tattoo '93 RAF Fairford The American Society of Mechanical Engineers I MECH E I NTERNATIONAL H ISTORIC M ECHANICAL E NGINEERING L ANDMARK PEGASUS V ECTORED-THRUST T URBOFAN ENGINE 1960 T HE B RISTOL AERO-ENGINES (ROLLS-R OYCE) PEGASUS ENGINE POWERED THE WORLD'S FIRST PRACTICAL VERTICAL/SHORT-TAKEOFF-AND-LANDING JET AIRCRAFT , THE H AWKER P. 1127 K ESTREL. USING FOUR ROTATABLE NOZZLES, ITS THRUST COULD BE DIRECTED DOWNWARD TO LIFT THE AIRCRAFT, REARWARD FOR WINGBORNE FLIGHT, OR IN BETWEEN TO ENABLE TRANSITION BETWEEN THE TWO FLIGHT REGIMES. T HIS ENGINE, SERIAL NUMBER BS 916, WAS PART OF THE DEVELOPMENT PROGRAM AND IS THE EARLIEST KNOWN SURVIVOR. PEGASUS ENGINE REMAIN IN PRODUCTION FOR THE H ARRIER II AIRCRAFT. T HE AMERICAN SOCIETY OF M ECHANICAL ENGINEERS T HE INSTITUTION OF M ECHANICAL ENGINEERS 1993 Evolution of the Pegasus Vectored-thrust Engine Introduction cern resulted in a perceived need trol and stability problems associ- The Pegasus vectored for combat runways for takeoff and ated with the transition from hover thrust engine provides the power landing, and which could, if re- to wing-borne flight. for the first operational vertical quired, be dispersed for operation The concepts examined and short takeoff and landing jet from unprepared and concealed and pursued to full-flight demon- aircraft. The Harrier entered ser- sites. Naval interest focused on a stration included "tail sitting" types vice with the Royal Air Force (RAF) similar objective to enable ship- exemplified by the Convair XFY-1 in 1969, followed by the similar borne combat aircraft to operate and mounted jet engines, while oth- AV-8A with the United States Ma- from helicopter-size platforms and ers used jet augmentation by means rine Corps in 1971. -
Pioneers to Partners, British Aircraft Since 1945
Pioneers to Partners British Aircraft since 1945 Christopher Foyle & Leo Marriott Foreword by Marshal of the Royal Air Force, HRH The Prince Philip, Duke of Edinburgh, KG, KT spsfojd |EuoiiEUJ9iu| JO(EW snojauunu in jguiJEd |Eiiu9ss9 PUE lUEiJodum UE s\ Xjisnpm UOjlEjAE IjSjljjg 31)1 9J9l|M UOjlEnijS UJ9pOLJU 91)1 01 iinds puE s9|i!)Euosj9d §uu99iioid uo iijnq Xjisnpui UE LJUOJJ 9§UEip ss9|iu9|9J inq 9|iqns 91)1 SUElp >|00q 91)1 '9)111 9lfl. Uj p91E|nsdEDU9 sy 'sdjijSJiB U9A9 puE sj9p||2 'si|mq-9uuoq p S||E19p j9Uq §U|A!§ S9D|pU9ddE l)l|M S|Enp!Alpll! plIE S9!UEdlUOD J9||EUUS 91)1 3-1 H U9HO§JOj 1O[\J uojinquiuoD JofEiu E 9pEUJ SEIJ /Jisnpin qsjiug 9J9qM s9iuuuEj2ojd |Euo!iEUJ9iui jo spnpojd 9SOLJ1 SE ||9M SE pOU3d IBljl UlljljM l^EJDJjE l|mq l)SI!Ug /J9A9JO 'J9pJO )ED!§0|OUOJl)D Uj 'S|jB13p SujpjAOjd Xq A'JOIS ai)i SujiEJisn)!! '/Ep iu9S9jd 91)1 01 c^6|, iiiojj AJisnpu! ^EJDJJE ijsiiug 91)1 Uj 9§UEl)D 91)1 SlJEljD SJ9UJJDJ OJ SJ33L/0/J 'lU9JEddE X||pE9J S/EM|E 10 u sj Xijiuspi qsjiug 3i|i q§noqi|E p9iu9S9jd9j ||9M 9J9M S1SJ1U9DS pUE SJ99U|§U9 'SgjUEduUOD l)SjlUg tpjljM Ul EI1JOSUOD IEUOJ1EUJ91UI Ol p9| S9UUlUEJ§Ojd lU9LJUdO|9A9p l^EJDJIE JOfEUU JO 1SOD pUE 9|EDS J991JS 91)1 X||EniU9Ag S9iEJ9uuo|§uoD lEUisnpuj J9§JE| oiui pgqjosqE X||EnpEJ§ 9J9M pUE||!AE|-) 9p pUE (OlSjjg 'OJA\/ SE ipns S9UUEU snouiiEj PUE Xjisnpui IJEJDJJE 3i)i UjqijM SUOHESJIEJUOIIEJ JOfElU Ol p9| XiqEUEAUj S9pED9p JEMlSOd 31)1 JO Xll|E9J 3l)_|_ 'SS9DDnS LjljM p9UMOJD SXEM|E 1OU 9J9M SIJOJ-P 9S91J1 E qi|M s|i)i uo p|inq 01 iqSnos PUE uo|S|ndojd 13 [ Uj J9pE9| p|JOM 91)1 -
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. -
Uk F-35B Srvl
8.)%659/ ,QIRUPDWLRQDW 'HF 23DJHVKDYHEHHQUHSULQWHGWRUHGXFHILOH VL]HWRXSORDGWRWKLVIRUXPPDNLQJWKHWH[W 85/VµGHDG¶KRZHYHUWKH85/WH[WUHPDLQV BRIEFING: SHIPBORNE have shown that the F-35B has a Sea State 6) requirement saw ROLLING VERTICAL LANDING critical vulnerability to deck mo- it ruled out on grounds of pilot tion for the SRVL manoeuvre. So workload and risk. So a stabi- [SRVL] c.2008 Richard Scott ZKLOHWKHUHLVFRQ¿GHQFHWKDW lised VLA quickly emerged as a SRVLs can he performed safely sine qua non. [SEA STATE 6: “4 to “...Landing aids in benign conditions with good 6 metres wave height - Very rough & With SRVL now likely to he used visibility, it was apparent that Surface Wind speed from Table can be as a primary recovery technique the real task drivers for the from 27-33 knots” Sea State Table: on board CVF, there is an addi- manoeuvre were higher sea http://www.syqwestinc.com/sup- tional requirement to augment states and night/poor weath- port/Sea%20State%20Table.htm the baseline landing aids suite er conditions.” & http://en.wikipedia.org/wiki/ with a landing aid appropriate to 6LPXODWRUÀ\LQJXQGHUWDNHQ Sea_state ] the SRVL approach manoeuvre. on both sides of the Atlantic, in- Existing systems were evalu- To this end QinetiQ has been cluding work at BAE Systems’ ated, including the US Navy’s contracted to research, concep- Warton Motion Dome Simulator Improved Fresnel Lens Optical tualise and prototype a new VLA in December 2007, had brought Landing System (IFOLS). “How- concept, known as the Bedford the problem into sharp relief. ever, the verdict on IFOLS was Array, which takes inputs “Quite simply, these simulations that it was reasonably expensive, from inertial references to showed that pilots would crash in not night-vision goggle compat- stabilise against deck mo- high sea state conditions without ible and, as a mechanical system, tions (pitch and heave). -
Eurofighter Review Issue 01/2006
programme news and features issue 1 - 2006 eurofighter review N DA1 Lands for the Last Time N 2005 Programme Review Eurofighter Typhoon Enters Final Stages of Flight Test N Eurofighter Typhoon In February, the Eurofighter Flight Test remaining clearances for the Phase 4 FCS undergo rigorous testing in all four Partner Team put Instrumented Production Aircraft will be finalised over the Summer. The final Nations and will involve six aircraft from Moves to the Three (IPA3) through several underwing stage of testing will be the validation of the the Flight Test fleet. heavy load tests, with four Paveway II Phase 5 air-to-ground FCS. The software, On conclusion, the final clearances for Front Line bombs, three external fuel tanks, and a written by a Joint Team headed by EADS the Full Operational Capability will be ex- complement of air-to-air missiles. Military Air Systems in Germany, will pected in 2007, followed by the availability These tests come as Eurofighter Typhoon of the Phase 5 software to Block 5 aircraft. opens the final chapter of the Main Develop- The first Block 5 Eurofighter Typhoon is ment Contract. The testing of the air-to-air already in final assembly in Germany, with carefree handling Flight Control Software deliveries of this standard of aircraft to (FCS) is almost finished, while the begin in early 2007. Performance is Key Programme Advances Through 2006 Eurofighter Typhoon IPA3 in under wing load tests as aircraft development enters the final stages 4 1 - 2006 eurofighter review contents - news - editorial - - editorial - 1 - 2006 eurofighter review 3 Contents Aloysius Rauen CEO Eurofighter GmbH 03 editorial Welcome note from Aloysius Rauen, Chief Executive Officer Dear Friends of Eurofighter Typhoon, 04 04 News Welcome to Eurofighter Review – the new Latest developments quarterly publication from Eurofighter. -
Front Cover: Airbus 2050 Future Concept Aircraft
AEROSPACE 2017 February 44 Number 2 Volume Society Royal Aeronautical www.aerosociety.com ACCELERATING INNOVATION WHY TODAY IS THE BEST TIME EVER TO BE AN AEROSPACE ENGINEER February 2017 PROPELLANTLESS SPACE DRIVES – FLIGHTS OF FANCY? BOOM PLOTS RETURN TO SUPERSONIC FLIGHT INDIA’S NAVAL AIR POWER Have you renewed your Membership Subscription for 2017? Your membership subscription was due on 1 January 2017. As per the Society’s Regulations all How to renew: membership benefits will be suspended where Online: a payment for an individual subscription has Log in to your account on the Society’s www.aerosociety.com not been received after three months of the due website to pay at . If you date. However, this excludes members paying do not have an account, you can register online their annual subscriptions by Direct Debits in and pay your subscription straight away. monthly installments. Additionally members Telephone: Call the Subscriptions Department who are entitled to vote in the Society’s AGM on +44 (0)20 7670 4315 / 4304 will lose their right to vote if their subscription has not been paid. Cheque: Cheques should be made payable to the Royal Aeronautical Society and sent to the Don’t lose out on your membership benefits, Subscriptions Department at No.4 Hamilton which include: Place, London W1J 7BQ, UK. • Your monthly subscription to AEROSPACE BACS Transfer: Pay by Bank Transfer (or by magazine BACS) into the Society’s bank account, quoting • Use of your RAeS post nominals as your name and membership number. Bank applicable details: • Over 400 global events yearly • Discounted rates for conferences Bank: HSBC plc • Online publications including Society News, Sort Code: 40-05-22 blogs and podcasts Account No: 01564641 • Involvement with your local branch BIC: MIDLGB2107K • Networking opportunities IBAN: GB52MIDL400522 01564641 • Support gaining Professional Registration • Opportunities & recognition with awards and medals • Professional development and support .. -
A HISTORY of IV (Army Co-Operation) Squadron
A HISTORY OF IV (Army Co-operation) Squadron 1912 - 2009 1 CONTENTS Battle Honours Page 3 Motto Page 4 Foreword Page 6 The Formative Years Page 7 World War 1 Page 9 The Inter-war Years Page 14 World War 2 Page 19 The Cold War Page 27 The Cold War – Harrier I Page 30 Post-Cold War – Harrier II Page 33 Post-9/11 Conflicts Page 35 Post Script Page 38 Members’ Recollections Page 39 Gate Guardian Page 50 Affiliations Page 51 Award of IV(AC) Sqn Standard Page 53 IV (AC) Sqn Bases Page 54 IV (AC) Sqn Aircraft Page 57 IV (AC) Sqn Commanding Officers Page 59 Age vs Seniority Page 60 Squadron Origins Page 61 2 BATTLE HONOURS IV(AC) Squadron Western Front 1914-1918 Mons Neuve Chappelle Somme 1916 Ypres 1917 Lys Somme 1918 France and Low Countries 1939-1940 Fortress Europe 1942-1945 France and Germany 1944-1945 Normandy 1944 Arnhem Rhine Iraq 2003 3 MOTTO IV(AC) Squadron The motto “In Futurum Videre” (To see into the future, or forward looking) refers to the Squadron’s reconnaissance role. The badge: ‘A sun in splendour divided by a flash of lightning’ was approved by HRH King Edward VIII in May 1936. The red and black segmented sun suggests “round the clock” operations while the lightning flash indicates speed and is also a reference to the unit’s early use of wireless telephony for artillery co-operation. 4 Squadron Personnel l914 Squadron Personnel 2009 5 FOREWORD By OC IV(AC) Squadron Wg Cdr H Smyth ‘…the man who looks back at history, goes forward with one eye blind; he who looks only to the future, goes forward blind in both eyes.’ (Russian Proverb) On the 16th September 2007, No IV(Army Co-operation) Squadron celebrated its 95th Anniversary. -
Additive Manufacturing Revives Hawker Typhoon Aircraft
Case study Additive manufacturing revives Hawker Typhoon aircraft Customer: Challenge: Solution: Jet Age Museum Accurately produce replacement Aluminium brackets brackets for the Hawker Typhoon using Renishaw’s AM250 Industry: aircraft cockpit. manufacturing system. Scientific, research and analysis For almost two decades, the Jet Age Museum in Gloucester, Only 3,317 Typhoons were ever made and there are very UK, has been working on bringing a Hawker Typhoon aircraft few around today; none are in flying condition. In 1998, when back to the city that originally manufactured it. Struggling an almost complete — but exceedingly corroded — cockpit to find engineering companies capable of recreating the section was found at a scrap yard in Wiltshire, volunteers complete brackets from the original 1938 drawings, which vowed to restore an aircraft with a rich national and regional were lacking manufacturing details, the museum got in touch importance. with Renishaw. We can’t put a price on what Renishaw has done for the Typhoon, the Eager to help, the global engineering Jet Age Museum and the local community. We would not have been able company produced the unconventional to reproduce these brackets without additive manufacturing technology brackets for the cockpit using the latest — the parts are too unconventional, a little bit like the Typhoon itself. By metal additive manufacturing (3D combining the old and new, Renishaw has helped keep a project started printing) technology, allowing the Typhoon in 1998 alive and well and has brought one of Britain’s iconic fighter restoration project to continue as planned. aircraft back home. Jet Age Museum (UK) Background Located just down the road from the birthplace of the Typhoon The Hawker Typhoon — or “Tiffy” as it was affectionately in Gloucester, the Jet Age Museum is pushing forward with referred to by the Royal Air Force (RAF) — was a British the project today. -
The Raf Harrier Story
THE RAF HARRIER STORY 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 2006: Royal Air Force Historical Society First published in the UK in 2006 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 0-9530345-2-6 Printed by Advance Book Printing Unit 9 Northmoor Park Church Road Northmoor OX29 5UH 3 ROYAL AIR FORCE HISTORICAL SOCIETY President Marshal of the Royal Air Force Sir Michael Beetham GCB CBE DFC AFC Vice-President Air Marshal Sir Frederick Sowrey KCB CBE AFC Committee Chairman Air Vice-Marshal N B Baldwin CB CBE FRAeS Vice-Chairman Group Captain J D Heron OBE Secretary Group Captain K J Dearman Membership Secretary Dr Jack Dunham PhD CPsychol AMRAeS Treasurer J Boyes TD CA Members Air Commodore H A Probert MBE MA *J S Cox Esq BA MA *Dr M A Fopp MA FMA FIMgt *Group Captain N Parton BSc (Hons) MA MDA MPhil CEng FRAeS RAF *Wing Commander D Robertson RAF Wing Commander C Cummings Editor & Publications Wing Commander C G Jefford MBE BA Manager *Ex Officio 4 CONTENTS EARLY HISTORICAL PERSPECTIVES AND EMERGING 8 STAFF TARGETS by Air Chf Mshl Sir Patrick Hine JET LIFT by Prof John F Coplin 14 EVOLUTION OF THE PEGASUS VECTORED