The F119 Engine: a Success Story of Human Systems Integration in Acquisition
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Eurofighter World Editorial 2016 • Eurofighter World 3
PROGRAMME NEWS & FEATURES DECEMBER 2016 GROSSETO EXCLUSIVE BALTIC AIR POLICING A CHANGING AIR FORCE FIT FOR THE FUTURE 2 2016 • EUROFIGHTER WORLD EDITORIAL 2016 • EUROFIGHTER WORLD 3 CONTENTS EUROFIGHTER WORLD PROGRAMME NEWS & FEATURES DECEMBER 2016 05 Editorial 24 Baltic policing role 42 Dardo 03 Welcome from Volker Paltzo, Germany took over NATO’s Journalist David Cenciotti was lucky enough to CEO of Eurofighter Jagdflugzeug GmbH. Baltic Air Policing (BAP) mis - get a back seat ride during an Italian Air Force sion in September with five training mission. Read his eye-opening first hand Eurofighters from the Tactical account of what life onboard the Eurofighter Title: Eurofighter Typoon with 06 At the heart of the mix Air Wing 74 in Neuburg, Typhoon is really like. P3E weapons fit. With the UK RAF evolving to meet new demands we speak to Bavaria deployed to Estonia. Typhoon Force Commander Air Commodore Ian Duguid about the Picture: Jamie Hunter changing shape of the Air Force and what it means for Typhoon. 26 Meet Sina Hinteregger By day Austrian Sina Hinteregger is an aircraft mechanic working on Typhoon, outside work she is one of the country’s best Eurofighter World is published by triathletes. We spoke to her Eurofighter Jagdflugzeug GmbH about her twin passions. 46 Power base PR & Communications Am Söldnermoos 17, 85399 Hallbergmoos Find out how Eurofighter Typhoon wowed the Tel: +49 (0) 811-80 1587 crowds at AIRPOWER16, Austria’s biggest Air [email protected] 12 Master of QRA Show. Editorial Team Discover why Eurofighter Typhoon’s outstanding performance and 28 Flying visit: GROSSETO Theodor Benien ability make it the perfect aircraft for Quick Reaction Alert. -
Why China Has Not Caught Up
Why China Has Not Caught Up Yet Why China Has Not Andrea Gilli and Caught Up Yet Mauro Gilli Military-Technological Superiority and the Limits of Imitation, Reverse Engineering, and Cyber Espionage Can adversaries of the United States easily imitate its most advanced weapon systems and thus erode its military-technological superiority? Do reverse engineering, industrial espi- onage, and, in particular, cyber espionage facilitate and accelerate this process? China’s decades-long economic boom, military modernization program, mas- sive reliance on cyber espionage, and assertive foreign policy have made these questions increasingly salient. Yet, almost everything known about this topic draws from the past. As we explain in this article, the conclusions that the ex- isting literature has reached by studying prior eras have no applicability to the current day. Scholarship in international relations theory generally assumes that ris- ing states beneªt from the “advantage of backwardness,” as described by Andrea Gilli is a senior researcher at the NATO (North Atlantic Treaty Organization) Defense College in Rome, Italy. Mauro Gilli is a senior researcher at the Center for Security Studies at the Swiss Federal Insti- tute of Technology in Zurich, Switzerland. The authors are listed in alphabetical order to reºect their equal contributions to this article. The views expressed in the article are those of the authors and do not represent the views of NATO, the NATO Defense College, or any other institution with which the authors are or have been -
Some Supersonic Aerodynamics
Some Supersonic Aerodynamics W.H. Mason Configuration Aerodynamics Class Grumman Tribody Concept – from 1978 Company Calendar The Key Topics • Brief history of serious supersonic airplanes – There aren’t many! • The Challenge – L/D, CD0 trends, the sonic boom • Linear theory as a starting point: – Volumetric Drag – Drag Due to Lift • The ac shift and cg control • The Oblique Wing • Aero/Propulsion integration • Some nonlinear aero considerations • The SST development work • Brief review of computational methods • Possible future developments Are “Supersonic Fighters” Really Supersonic? • If your car’s speedometer goes to 120 mph, do you actually go that fast? • The official F-14A supersonic missions (max Mach 2.4) – CAP (Combat Air Patrol) • 150 miles subsonic cruise to station • Loiter • Accel, M = 0.7 to 1.35, then dash 25nm – 4 ½ minutes and 50nm total • Then, head home or to a tanker – DLI (Deck Launch Intercept) • Energy climb to 35K ft., M = 1.5 (4 minutes) • 6 minutes at 1.5 (out 125-130nm) • 2 minutes combat (slows down fast) After 12 minutes, must head home or to a tanker Very few real supersonic airplanes • 1956: the B-58 (L/Dmax = 4.5) – In 1962: Mach 2 for 30 minutes • 1962: the A-12 (SR-71 in ’64) (L/Dmax = 6.6) – 1st supersonic flight, May 4, 1962 – 1st flight to exceed Mach 3, July 20, 1963 • 1964: the XB-70 (L/Dmax = 7.2) – In 1966: flew Mach 3 for 33 minutes • 1968: the TU-144 – 1st flight: Dec. 31, 1968 • 1969: the Concorde (L/Dmax = 7.4) – 1st flight, March 2, 1969 • 1990: the YF-22 and YF-23 (supercruisers) – YF-22: 1st flt. -
10. Supersonic Aerodynamics
Grumman Tribody Concept featured on the 1978 company calendar. The basis for this idea will be explained below. 10. Supersonic Aerodynamics 10.1 Introduction There have actually only been a few truly supersonic airplanes. This means airplanes that can cruise supersonically. Before the F-22, classic “supersonic” fighters used brute force (afterburners) and had extremely limited duration. As an example, consider the two defined supersonic missions for the F-14A: F-14A Supersonic Missions CAP (Combat Air Patrol) • 150 miles subsonic cruise to station • Loiter • Accel, M = 0.7 to 1.35, then dash 25 nm - 4 1/2 minutes and 50 nm total • Then, must head home, or to a tanker! DLI (Deck Launch Intercept) • Energy climb to 35K ft, M = 1.5 (4 minutes) • 6 minutes at M = 1.5 (out 125-130 nm) • 2 minutes Combat (slows down fast) After 12 minutes, must head home or to a tanker. In this chapter we will explain the key supersonic aerodynamics issues facing the configuration aerodynamicist. We will start by reviewing the most significant airplanes that had substantial sustained supersonic capability. We will then examine the key physical underpinnings of supersonic gas dynamics and their implications for configuration design. Examples are presented showing applications of modern CFD and the application of MDO. We will see that developing a practical supersonic airplane is extremely demanding and requires careful integration of the various contributing technologies. Finally we discuss contemporary efforts to develop new supersonic airplanes. 10.2 Supersonic “Cruise” Airplanes The supersonic capability described above is typical of most of the so-called supersonic fighters, and obviously the supersonic performance is limited. -
A Supersonic Fan Equipped Variable Cycle Engine for a Mach 2.7 Supersonic Transport
University of New Hampshire University of New Hampshire Scholars' Repository Applied Engineering and Sciences Scholarship Applied Engineering and Sciences 8-22-1985 A Supersonic Fan Equipped Variable Cycle Engine for a Mach 2.7 Supersonic Transport Theodore S. Tavares University of New Hampshire, Manchester, [email protected] Follow this and additional works at: https://scholars.unh.edu/unhmcis_facpub Recommended Citation Tavares, T.S., “A Supersonic Fan Equipped Variable Cycle Engine for a Mach 2.7 Supersonic Transport,” NASA-CR-177141, 1986. This Report is brought to you for free and open access by the Applied Engineering and Sciences at University of New Hampshire Scholars' Repository. It has been accepted for inclusion in Applied Engineering and Sciences Scholarship by an authorized administrator of University of New Hampshire Scholars' Repository. For more information, please contact [email protected]. https://ntrs.nasa.gov/search.jsp?R=19860019474 2018-07-25T19:53:49+00:00Z ^4/>*>?/ GAS TURBINE LABORATORY DEPARTMENT OF AERONAUTICS AND ASTRONAUTICS MASSACHUSETTS INSTITUTE OF TECHNOLOGY CAMBRIDGE, MA 02139 A FINAL REPORT ON NASA GRANT NAG-3-697 entitled A SUPERSONIC FAN EQUIPPED VARIABLE CYCLE ENGINE FOR A MACH 2.7 SUPERSONIC TRANSPORT by T. S. Tavares prepared for NASA Lewis Research Center Cleveland, OH 44135 (NASA-CB-177141) A SDPEBSCNIC FAN EQUIPPED N86-28946 VARIABLE CYCLE ENGINE.JOB A MACH 2.? SDPEESONIC TBANSPOBT Final Report (Massachusetts Inst. of Tech.) 107 p Unclas CSCL 21E G3/07 43461 August 22, 1985 A SUPERSONIC FAN EQUIPPED VARIABLE CYCLE ENGINE FOR A HACK 2.7 SUPERSONIC TRANSPORT by Theodore Sean Tavares A SUPERSONIC FAN EQUIPPED VARIABLE CYCLE ENGINE FOR A MACH 2.7 SUPERSONIC TRANSPORT by THEODORE SEAN TAVARES ABSTRACT A design stud/ was carried out to evaluate the concept of a variable cycle turbofan engine with an axially supersonic fan stage as powerplant for a Mach 2.7 supersonic transport. -
The Power for Flight: NASA's Contributions To
The Power Power The forFlight NASA’s Contributions to Aircraft Propulsion for for Flight Jeremy R. Kinney ThePower for NASA’s Contributions to Aircraft Propulsion Flight Jeremy R. Kinney Library of Congress Cataloging-in-Publication Data Names: Kinney, Jeremy R., author. Title: The power for flight : NASA’s contributions to aircraft propulsion / Jeremy R. Kinney. Description: Washington, DC : National Aeronautics and Space Administration, [2017] | Includes bibliographical references and index. Identifiers: LCCN 2017027182 (print) | LCCN 2017028761 (ebook) | ISBN 9781626830387 (Epub) | ISBN 9781626830370 (hardcover) ) | ISBN 9781626830394 (softcover) Subjects: LCSH: United States. National Aeronautics and Space Administration– Research–History. | Airplanes–Jet propulsion–Research–United States– History. | Airplanes–Motors–Research–United States–History. Classification: LCC TL521.312 (ebook) | LCC TL521.312 .K47 2017 (print) | DDC 629.134/35072073–dc23 LC record available at https://lccn.loc.gov/2017027182 Copyright © 2017 by the National Aeronautics and Space Administration. The opinions expressed in this volume are those of the authors and do not necessarily reflect the official positions of the United States Government or of the National Aeronautics and Space Administration. This publication is available as a free download at http://www.nasa.gov/ebooks National Aeronautics and Space Administration Washington, DC Table of Contents Dedication v Acknowledgments vi Foreword vii Chapter 1: The NACA and Aircraft Propulsion, 1915–1958.................................1 Chapter 2: NASA Gets to Work, 1958–1975 ..................................................... 49 Chapter 3: The Shift Toward Commercial Aviation, 1966–1975 ...................... 73 Chapter 4: The Quest for Propulsive Efficiency, 1976–1989 ......................... 103 Chapter 5: Propulsion Control Enters the Computer Era, 1976–1998 ........... 139 Chapter 6: Transiting to a New Century, 1990–2008 .................................... -
Turbomachinery Technology for High-Speed Civil Flight
4 NASA Technical Memorandum 102092 . Turbomachinery Technology for High-speed Civil Flight , Neal T. Saunders and Arthur J. Gllassman Lewis Research Center Cleveland, Ohio Prepared for the 34th International Gas Turbine Aepengine Congress and Exposition sponsored by the American Society of Mechanical Engineers Toronto, Canada, June 4-8, 1989 ~ .. (NASA-TH-102092) TURBOHACHINERY TECHPCLOGY N89-24320 FOR HIGH-SPEED CIVIL FLIGHT (NBSEL, LEV& Research Center) 26 p CSCL 21E Unclas G3/07 0217641 TURBOMACHINERY TECHNOLOGY FOR HIGH-SPEED CIVIL FLIGHT Neal T. Saunders and Arthur J. Glassman ABSTRACT This presentation highlights some of the recent contributions and future directions of NASA Lewis Research Center's research and technology efforts applicable to turbomachinery for high-speed flight. For a high-speed civil transport application, the potential benefits and cycle requirements for advanced variable cycle engines and the supersonic throughflow fan engine are presented. The supersonic throughf low fan technology program is discussed. Technology efforts in the basic discipline areas addressing the severe operat- ing conditions associated with high-speed flight turbomachinery are reviewed. Included are examples of work in internal fluid mechanics, high-temperature materials, structural analysis, instrumentation and controls. c INTRODUCTION Future Emphasis Shifting to High-speed Flight Two years ago, the aeronautics community commemorated the 50th anniversary of the first successful operation of a turbojet engine. This remarkable feat by Sir Frank Whittle represents the birth of the turbine engine industry, which has greatly refined and improved Whittle's invention into the splendid engines that are flying today. NASA, as did its predecessor NACA, has assisted indus- try in the creation and development of advanced technologies for each new gen- eration of engines. -
Milestonesofmannedflight World
' J/ILESTONES of JfANNED i^LIGHT With a short dash down the runway, the machine lifted into the air and was flying. It was only a flight of twelve seconds, and it was an uncertain, waiy. creeping sort offlight at best: but it was a realflight at last and not a glide. ORV1U.E VPRK.HT A DIRECT RESULT OF OnUle Wright's intrepid 12- second A flight on Kill Devil Hill in 1903. mankind, in the space of just nine decades, has developed the means to leave the boundaries of Earth, visit space and return. As a matter of routine, even- )ear millions of business people and tourists travel to the furthest -^ reaches of our planet within a matter of hours - some at twice the speed of sound. The progress has, quite simpl) . been astonishing. Having discovered the means of controlled flight in a powered, heavier-than-air machine, other uses than those of transpon were inevitable and research into the militan- potential of manned flight began almost immediatel>-. The subsequent effect of aviation on warfare has been nothing shon of revolutionary', and in most of the years since 1903 the leading technological innovations have resulted from militan- research programs. In Milestones of Manned Flight, aviation expen Mike .Spick has selected the -iO-plus events, both civil and militan-, which he considers to mark the most significant points of aviation histon-. Each one is illustrated, and where there have been significant related developments from that particular milestone, then these are featured too. From the intrepid and pioneering Wright brothers to the high-technology' gurus developing the F-22 Advanced Tactical Fighter, the histon' of manned flight is. -
Flight Line the Official Publication of the CAF Southern California Wing 455 Aviation Drive, Camarillo, CA 93010 (805) 482-0064
Flight Line The Official Publication of the CAF Southern California Wing 455 Aviation Drive, Camarillo, CA 93010 (805) 482-0064 May, 2016 Vol. XXXV No. 5 © Photo by Gene O’Neal Unveiling of Photo of So Cal Wing’s Spitfire displayed Visit us online at www.cafsocal.com in the Crown & Anchor, a Ventura County British pub. © Photo by Dan Newcomb Our CAF-So Cal Wing fighters, accompanied by Jason Somes’s Aero L-29 Delfin jet trainer flying in formation to the air show at March Air Force Base earlier this year. Wing Staff Meeting, Saturday, May 21, 2016 at 9:30 a.m. at the CAF Museum Hangar, 455 Aviation Drive, Camarillo Airport THE CAF IS A PATRIOTIC ORGANIZATION DEDICATED TO THE PRESERVATION OF THE WORLD’S GREATEST COMBAT AIRCRAFT. May 2016 Sunday Monday Tuesday Wednesday Thursday Friday Saturday 1 2 3 4 5 6 7 Museum Closed Work Day Work Day April Fool's Work Day Day 8 9 10 11 12 13 14 Museum Closed Work Day Work Day Work Day Mother's Day 15 16 17 18 19 20 21 Museum Closed Work Day Work Day Wing Staff Meeting 9:30 Work Day 22 23 24 25 26 27 28 Museum Closed Work Day Work Day Work Day Docent Meeting 12:00 29 30 31 Museum Open Museum Closed Work Day 10am to 4pm Every Day Except Monday Memorial Day and major holidays STAFF AND APPOINTED POSITIONS IN THIS ISSUE Wing Leader * Ron Missildine (805) 404-1837 [email protected] Wing Calendar . 2 Executive Officer * Steve Barber (805) 302-8517 exo@ cafsocal.com Staff and Appointed Positions. -
A High-Fidelity Approach to Conceptual Design John Thomas Watson Iowa State University
Iowa State University Capstones, Theses and Graduate Theses and Dissertations Dissertations 2016 A high-fidelity approach to conceptual design John Thomas Watson Iowa State University Follow this and additional works at: https://lib.dr.iastate.edu/etd Part of the Aerospace Engineering Commons, and the Art and Design Commons Recommended Citation Watson, John Thomas, "A high-fidelity approach to conceptual design" (2016). Graduate Theses and Dissertations. 15183. https://lib.dr.iastate.edu/etd/15183 This Thesis is brought to you for free and open access by the Iowa State University Capstones, Theses and Dissertations at Iowa State University Digital Repository. It has been accepted for inclusion in Graduate Theses and Dissertations by an authorized administrator of Iowa State University Digital Repository. For more information, please contact [email protected]. A high-fidelity approach to conceptual design by John T. Watson A thesis submitted to the graduate faculty in partial fulfillment of the requirements for the degree of MASTER OF SCIENCE Major: Aerospace Engineering Program of Study Committee: Richard Wlezien, Major Professor Thomas Gielda Leifur Leifsson Iowa State University Ames, Iowa 2016 Copyright © John T. Watson, 2016. All rights reserved. ii TABLE OF CONTENTS Page LIST OF FIGURES ................................................................................................... iii LIST OF TABLES ..................................................................................................... v NOMENCLATURE ................................................................................................. -
J-20 Stealth Fighter: China's First Strike Weapon
Foreign Affairs, Defence and Trade Committee Joint Strike Fighter Inquiry Department of the Senate PO Box 6100 Parliament House Canberra ACT 2600 Dear Chairman and Committee Members The Planned Acquisition of the F-35A Joint Strike Fighter Please find following my submission to this Inquiry. Yours faithfully, David Archibald Submission to the Joint Strike Fighter Inquiry Table of Contents Page 1. Executive Summary 2 2. Australia’s Future Air Defence Needs 3 3. Costs and Benefits of the F-35 Program 6 4. Changes in the Acquisition Timeline 7 5. The Performance of the F-35 in Testing 13 5.1 Introduction to the deficiencies of the F-35 13 5.2 Basing 18 5.3 Fuel Temperature 21 5.4 Engine 23 5.5 Acquisition Cost 24 5.6 Operating Cost 26 5.7 Directed Energy Weapon 28 5.8 DAS-EOTS 28 5.9 Manoeuvrability 29 5.10 Maintenance 31 5.11 Software 33 5.12 Pilot Training 33 5.13 Helmet Failure 34 5.14 Block Buy Contract 35 5.15 Stealth 35 5.16 Autonomic Logistics Information System 36 6. Potential Alternatives to the F-35 38 6.1 The Evolution of Fighter Aircraft 38 6.2 Fighter design considerations 39 6.3 How To Win In Air-To-Air Combat 45 6.4 Graphical Representation of Aircraft Attributes 46 6.5 Discussion of Alternatives to the F-35 56 6.6 F-18 Super Hornet 58 6.7 Gripen E 58 7. Any Other Related Matters 62 7.1 Basing and Logistics 62 7.2 Maintenance 62 7.3 Interim Aircraft 62 7.4 Aging of the F/A-18 A/B Hornet Aircraft 62 7.5 The US – Australia Alliance 64 8. -
Army Fires Capabilities for 2025 and Beyond
Army Fires Capabilities for 2025 and Beyond John Gordon IV, Igor Mikolic-Torreira, D. Sean Barnett, Katharina Ley Best, Scott Boston, Dan Madden, Danielle C. Tarraf, Jordan Willcox C O R P O R A T I O N For more information on this publication, visit www.rand.org/t/RR2124 Library of Congress Cataloging-in-Publication Data is available for this publication. ISBN: 978-0-8330-9967-9 Published by the RAND Corporation, Santa Monica, Calif. © Copyright 2019 RAND Corporation R® is a registered trademark. Cover: Army photo by Spc. Josselyn Fuentes. Limited Print and Electronic Distribution Rights This document and trademark(s) contained herein are protected by law. This representation of RAND intellectual property is provided for noncommercial use only. Unauthorized posting of this publication online is prohibited. Permission is given to duplicate this document for personal use only, as long as it is unaltered and complete. Permission is required from RAND to reproduce, or reuse in another form, any of its research documents for commercial use. For information on reprint and linking permissions, please visit www.rand.org/pubs/permissions. The RAND Corporation is a research organization that develops solutions to public policy challenges to help make communities throughout the world safer and more secure, healthier and more prosperous. RAND is nonprofit, nonpartisan, and committed to the public interest. RAND’s publications do not necessarily reflect the opinions of its research clients and sponsors. Support RAND Make a tax-deductible charitable contribution at www.rand.org/giving/contribute www.rand.org Preface This report documents research and analysis conducted as part of a project entitled Army Fires for Army 2025, sponsored by the Field Artil- lery School at Fort Sill, Oklahoma (a part of the U.S.