Air University Review: July-Augus 1968, Volume XIX, No. 5
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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. -
Shelf List 05/31/2011 Matches 4631
Shelf List 05/31/2011 Matches 4631 Call# Title Author Subject 000.1 WARBIRD MUSEUMS OF THE WORLD EDITORS OF AIR COMBAT MAG WAR MUSEUMS OF THE WORLD IN MAGAZINE FORM 000.10 FLEET AIR ARM MUSEUM, THE THE FLEET AIR ARM MUSEUM YEOVIL, ENGLAND 000.11 GUIDE TO OVER 900 AIRCRAFT MUSEUMS USA & BLAUGHER, MICHAEL A. EDITOR GUIDE TO AIRCRAFT MUSEUMS CANADA 24TH EDITION 000.2 Museum and Display Aircraft of the World Muth, Stephen Museums 000.3 AIRCRAFT ENGINES IN MUSEUMS AROUND THE US SMITHSONIAN INSTITUTION LIST OF MUSEUMS THROUGH OUT THE WORLD WORLD AND PLANES IN THEIR COLLECTION OUT OF DATE 000.4 GREAT AIRCRAFT COLLECTIONS OF THE WORLD OGDEN, BOB MUSEUMS 000.5 VETERAN AND VINTAGE AIRCRAFT HUNT, LESLIE LIST OF COLLECTIONS LOCATION AND AIRPLANES IN THE COLLECTIONS SOMEWHAT DATED 000.6 VETERAN AND VINTAGE AIRCRAFT HUNT, LESLIE AVIATION MUSEUMS WORLD WIDE 000.7 NORTH AMERICAN AIRCRAFT MUSEUM GUIDE STONE, RONALD B. LIST AND INFORMATION FOR AVIATION MUSEUMS 000.8 AVIATION AND SPACE MUSEUMS OF AMERICA ALLEN, JON L. LISTS AVATION MUSEUMS IN THE US OUT OF DATE 000.9 MUSEUM AND DISPLAY AIRCRAFT OF THE UNITED ORRISS, BRUCE WM. GUIDE TO US AVIATION MUSEUM SOME STATES GOOD PHOTOS MUSEUMS 001.1L MILESTONES OF AVIATION GREENWOOD, JOHN T. EDITOR SMITHSONIAN AIRCRAFT 001.2.1 NATIONAL AIR AND SPACE MUSEUM, THE BRYAN, C.D.B. NATIONAL AIR AND SPACE MUSEUM COLLECTION 001.2.2 NATIONAL AIR AND SPACE MUSEUM, THE, SECOND BRYAN,C.D.B. MUSEUM AVIATION HISTORY REFERENCE EDITION Page 1 Call# Title Author Subject 001.3 ON MINIATURE WINGS MODEL AIRCRAFT OF THE DIETZ, THOMAS J. -
Aerospace Dimensions Leader's Guide
Leader Guide www.capmembers.com/ae Leader Guide for Aerospace Dimensions 2011 Published by National Headquarters Civil Air Patrol Aerospace Education Maxwell AFB, Alabama 3 LEADER GUIDES for AEROSPACE DIMENSIONS INTRODUCTION A Leader Guide has been provided for every lesson in each of the Aerospace Dimensions’ modules. These guides suggest possible ways of presenting the aerospace material and are for the leader’s use. Whether you are a classroom teacher or an Aerospace Education Officer leading the CAP squadron, how you use these guides is up to you. You may know of different and better methods for presenting the Aerospace Dimensions’ lessons, so please don’t hesitate to teach the lesson in a manner that works best for you. However, please consider covering the lesson outcomes since they represent important knowledge we would like the students and cadets to possess after they have finished the lesson. Aerospace Dimensions encourages hands-on participation, and we have included several hands-on activities with each of the modules. We hope you will consider allowing your students or cadets to participate in some of these educational activities. These activities will reinforce your lessons and help you accomplish your lesson out- comes. Additionally, the activities are fun and will encourage teamwork and participation among the students and cadets. Many of the hands-on activities are inexpensive to use and the materials are easy to acquire. The length of time needed to perform the activities varies from 15 minutes to 60 minutes or more. Depending on how much time you have for an activity, you should be able to find an activity that fits your schedule. -
FAA Order 8130.2H, February 4, 2015
U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADM INISTRATION ORDER 8130.2H 02/04/2015 National Policy SUBJ: Airworthiness Certification of Products and Articles This order establishes procedures for accomplishing original and recurrent airworthiness certification ofaircraft and related products and articles. The procedures contained in this order apply to Federal Aviation Administration (FAA) manufacturing aviation safety inspectors (ASI), to FAA airworthiness AS Is, and to private persons or organizations delegated authority to issue airworthiness certificates and related approvals. Suggestions for improvement of this order may be submitted using the FAA Office of Aviation Safety (AVS) directive feedback system at http://avsdfs.avs.faa.gov/default.aspx, or FAA Form 1320-19, Directive Feedback Information, found in appendix I to this order. D G!JD Cf1 · ~ David Hempe Manager, Design, Manufacturing, & Airworthiness Division Aircraft Certification Service Distribution: Electronic Initiated By: AIR-1 00 02/04/2015 8130.2H Table of Contents Paragraph Page Chapter 1. Introduction 100. Purpose of This Order .............................................................................. 1-1 101. Audience .................................................................................................. 1-1 102. Where Can I Find This Order .................................................................. 1-1 103. Explanation of Policy Changes ................................................................ 1-1 104. Cancellation ............................................................................................ -
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. -
Warfare in a Fragile World: Military Impact on the Human Environment
Recent Slprt•• books World Armaments and Disarmament: SIPRI Yearbook 1979 World Armaments and Disarmament: SIPRI Yearbooks 1968-1979, Cumulative Index Nuclear Energy and Nuclear Weapon Proliferation Other related •• 8lprt books Ecological Consequences of the Second Ihdochina War Weapons of Mass Destruction and the Environment Publish~d on behalf of SIPRI by Taylor & Francis Ltd 10-14 Macklin Street London WC2B 5NF Distributed in the USA by Crane, Russak & Company Inc 3 East 44th Street New York NY 10017 USA and in Scandinavia by Almqvist & WikseH International PO Box 62 S-101 20 Stockholm Sweden For a complete list of SIPRI publications write to SIPRI Sveavagen 166 , S-113 46 Stockholm Sweden Stoekholol International Peace Research Institute Warfare in a Fragile World Military Impact onthe Human Environment Stockholm International Peace Research Institute SIPRI is an independent institute for research into problems of peace and conflict, especially those of disarmament and arms regulation. It was established in 1966 to commemorate Sweden's 150 years of unbroken peace. The Institute is financed by the Swedish Parliament. The staff, the Governing Board and the Scientific Council are international. As a consultative body, the Scientific Council is not responsible for the views expressed in the publications of the Institute. Governing Board Dr Rolf Bjornerstedt, Chairman (Sweden) Professor Robert Neild, Vice-Chairman (United Kingdom) Mr Tim Greve (Norway) Academician Ivan M£ilek (Czechoslovakia) Professor Leo Mates (Yugoslavia) Professor -
Leading the Charge We Put TBM 940 Speedster Through Its Paces for NBAA
15-21 October 2019 I flightglobal.com FLIGHT TEST Leading the charge We put TBM 940 speedster through its paces for NBAA £3.90 Wow, how? ACES high 42 Questions remain over defunct US Air Force boosts Collins Icelandic carrier’s comeback 13 with ejection seat deal 20 9 770015 371310 FLIGHT TEST Power of one Turboprop-single family has been a market success since launch in 1988, amassing sales of more than 900 units across three variants Daher has delivered a compelling offer for owner-flyers, with a range of enhancements on the TBM 940 providing an edge over the piston-twin segment. We put it through its paces MICHAEL GERZANICS POMPANO BEACH have allowed single-engined designs to make to be efficient. Airspace congestion, however, inroads into the twin-turbine segment. can make reaching optimum altitudes for jets he single-engined turboprop market The growth of the single-engined turbo- problematic, so their real-world range can be is populated by numerous aircraft of prop segment is based on the near-bulletproof shorter. Jets also have higher direct operating varying configurations. In broad reliability and scalability of the PT6 family. costs, however. T strokes, it can be broken down into This paradigm shift from piston-twins to tur- Runway performance and training require- two segments: fast, low-winged aircraft and bine-singles is conceptually on par with ex- ments are also two factors that fuel the single- slower, more spacious high-winged designs. tended twin-engine operations authorisations engined turboprop segment, because runway In the West, these diverse offerings share a all but killing off three- and four-engined civil length for turboprops is shorter than that single critical component – their engine. -
Executive Summary
The Boston University Astronomy Department Annual Report 2010 Chair: James Jackson Administrator: Laura Wipf 1 2 TABLE OF CONTENTS Executive Summary 5 Faculty and Staff 5 Teaching 6 Undergraduate Programs 6 Observatory and Facilities 8 Graduate Program 9 Colloquium Series 10 Alumni Affairs/Public Outreach 10 Research 11 Funding 12 Future Plans/Departmental Needs 13 APPENDIX A: Faculty, Staff, and Graduate Students 16 APPENDIX B: 2009/2010 Astronomy Graduates 18 APPENDIX C: Seminar Series 19 APPENDIX D: Sponsored Project Funding 21 APPENDIX E: Accounts Income Expenditures 25 APPENDIX F: Publications 27 Cover photo: An ultraviolet image of Saturn taken by Prof. John Clarke and his group using the Hubble Space Telescope. The oval ribbons toward the top and bottom of the image shows the location of auroral activity near Saturn’s poles. This activity is analogous to Earth’s aurora borealis and aurora australis, the so-called “northern” and “southern lights,” and is caused by energetic particles from the sun trapped in Saturn’s magnetic field. 3 4 EXECUTIVE SUMMARY associates authored or co-authored a total of 204 refereed, scholarly papers in the disciplines’ most The Department of Astronomy teaches science to prestigious journals. hundreds of non-science majors from throughout the university, and runs one of the largest astronomy degree The funding of the Astronomy Department, the Center programs in the country. Research within the for Space Physics, and the Institute for Astrophysical Astronomy Department is thriving, and we retain our Research was changed this past year. In previous years, strong commitment to teaching and service. only the research centers received research funding, but last year the Department received a portion of this The Department graduated a class of twelve research funding based on grant activity by its faculty. -
A Harrier GR.9, ZD 406, Royal Navy Naval Strike Wing, RAF Station Cottesmore, 2009
Harrier GR.7/9 BRITISH FIGHTER 1/48 SCALE PLASTIC KIT #1166 INTRO The development of precision-attack missiles with a nuclear warhead during the 1950s changed strategic military doctrine dramatically. It became obvious that large military air bases would become easy targets that could be wiped out by a single, precise strike. This prompted French aircraft designer Michel Wibault to wonder, in 1955, if NATO might not be making a mistake by constructing some 100 new 'field' bases called Basic Operational Platforms (BOP) alongside the border of the Eastern Block. Instead, Whibault proposed the development of an aircraft with VTOL (Vertical Take-off and Landing) capability, eliminating the need for the proposed air bases. First drawings The VTOL (Vertical Take off and Landing) concept is not a new idea. Several VTOL aircraft were proposed during World War II, but it was the dawn of the jet era that brought new possibilities, first tested with Rolls-Royces´ Bedstead flying device. A real aircraft followed in the form of the Short SC.1 prototype, using four RB.108 turbojets pointing downward with a fifth pointing to the rear for forward propulsion, but it was quite obvious such a layout was ineffective. Instead, Wibault proposed a single powerful gas turbine, driving four high-capacity movable blowers via shafts. There was not too much interest at Dassault, but it attracted the attention of USAF colonel Johnny Driscoll, who was then commander of the Paris based MWDP (Mutual Weapons Development Program). He presented Wibaults´ plans to Theodore von Karman and the famous engineer and physicist was impressed. -
Hadley's Principle: Understanding and Misunderstanding the Trade
History of Meteorology 3 (2006) 17 Hadley’s Principle: Understanding and Misunderstanding the Trade Winds Anders O. Persson Department for research and development Swedish Meteorological and Hydrological Institute SE 601 71 Norrköping, Sweden [email protected] Old knowledge will often be rediscovered and presented under new labels, causing much confusion and impeding progress—Tor Bergeron.1 Introduction In May 1735 a fairly unknown Englishman, George Hadley, published a groundbreaking paper, “On the Cause of the General Trade Winds,” in the Philosophical Transactions of the Royal Society. His path to fame was long and it took 100 years to have his ideas accepted by the scientific community. But today there is a “Hadley Crater” on the moon, the convectively overturning in the tropics is called “The Hadley Cell,” and the climatological centre of the UK Meteorological Office “The Hadley Centre.” By profession a lawyer, born in London, George Hadley (1685-1768) had in 1735 just became a member of the Royal Society. He was in charge of the Society’s meteorological work which consisted of providing instruments to foreign correspondents and of supervising, collecting and scrutinizing the continental network of meteorological observations2. This made him think about the variations in time and geographical location of the surface pressure and its relation to the winds3. Already in a paper, possibly written before 1735, Hadley carried out an interesting and far-sighted discussion on the winds, which he found “of so uncertain and variable nature”: Hadley’s Principle 18 …concerning the Cause of the Trade-Winds, that for the same Cause the Motion of the Air will not be naturally in a great Circle, for any great Space upon the surface of the Earth anywhere, unless in the Equator itself, but in some other Line, and, in general, all Winds, as they come nearer the Equator will become more easterly, and as they recede from it, more and more westerly, unless some other Cause intervene4. -
Viscosity from Newton to Modern Non-Equilibrium Statistical Mechanics
Viscosity from Newton to Modern Non-equilibrium Statistical Mechanics S´ebastien Viscardy Belgian Institute for Space Aeronomy, 3, Avenue Circulaire, B-1180 Brussels, Belgium Abstract In the second half of the 19th century, the kinetic theory of gases has probably raised one of the most impassioned de- bates in the history of science. The so-called reversibility paradox around which intense polemics occurred reveals the apparent incompatibility between the microscopic and macroscopic levels. While classical mechanics describes the motionof bodies such as atoms and moleculesby means of time reversible equations, thermodynamics emphasizes the irreversible character of macroscopic phenomena such as viscosity. Aiming at reconciling both levels of description, Boltzmann proposed a probabilistic explanation. Nevertheless, such an interpretation has not totally convinced gen- erations of physicists, so that this question has constantly animated the scientific community since his seminal work. In this context, an important breakthrough in dynamical systems theory has shown that the hypothesis of microscopic chaos played a key role and provided a dynamical interpretation of the emergence of irreversibility. Using viscosity as a leading concept, we sketch the historical development of the concepts related to this fundamental issue up to recent advances. Following the analysis of the Liouville equation introducing the concept of Pollicott-Ruelle resonances, two successful approaches — the escape-rate formalism and the hydrodynamic-mode method — establish remarkable relationships between transport processes and chaotic properties of the underlying Hamiltonian dynamics. Keywords: statistical mechanics, viscosity, reversibility paradox, chaos, dynamical systems theory Contents 1 Introduction 2 2 Irreversibility 3 2.1 Mechanics. Energyconservationand reversibility . ........................ 3 2.2 Thermodynamics. -
CF-18 Fighter Demonstration Manual
FIGHTER DEMONSTRATION MANUAL Version 4.0 Issued under the Authority of Commander 1 Canadian Air Division Custodian: OC FSET March 2019 Endorsed by: Approved by: Recoverable Signature Recoverable Signature X A DComd FG Col Luc Girou... X BGen I.H. Huddleston MGen J.H.C Drouin Deputy Commander Force Generation Commander 1 Canadian Air Division Signed by: GIROUARD, LUC 607 Signed by: BOYLE, SEAN 627 Fighter Demonstration Manual Record of Amendments Amend DATE DETAILS DONE BY # 0 XX Mar 19 Capt Thys R.G.T. This document is issued on the authority of the OC Fighter Standards and Evaluation Team (FSET) and contains information specific to the employment and role of the Fighter Demonstration Team. Inquiries and suggestions for changes shall be forwarded through Special Events Coord and OC FSET for review and submission to SSO Fighters for the approval of the Commander 1 Canadian Air Division. Table of Contents FIGHTER DEMONSTRATION MANUAL .................................................... 1 Chapter 1: PREPARATION ........................................................................ 8 101. TEAM SELECTION ........................................................... 8 102. AIRSHOW ROUTINE ........................................................ 9 103. FIGHTER DEMONSTRATION TRAINING ........................ 9 104. ACCEPTANCE SHOW ...................................................... 9 Chapter 2: OPERATIONAL CONSIDERATIONS .................................... 11 201. CONFIGURATION .......................................................... 11