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Parking Speed Its Own Mighty Sound and Sights Dis- Spring Morning in 1988
was behind the wheel, I am complete- ly confident that anything about the day the sound barrier fell on that des- olate stretch of the Black Rock Desert in Nevada, is as good as technology yy can recreate it. How fast these past seven years have flown by. I still marvel at how the guy never shut-up while driving. When the car yy was moving, Green was always talk- ing, calm and cool as if he were a commercial airplane pilot giving you his cockpit spiel – his voice never wavered, even when he lost both yyFuel For Thought parachutes at 714MPH! Got to be the fighter pilot training in him. with “Landspeed Louise” Ann Noeth Also in the ‘Spirit of Speed’ gallery Trudy and Mickey Thompson as the is Richard Nobles’ jet ride Thrust 2 world will forever remember them . which set the World Land Speed before they were gunned down by vile yy Record at 633MPH in 1984, which has cowards in front of their home early one Parking Speed its own mighty sound and sights dis- Spring morning in 1988. play. Thrust 2 and team had tried to Coventry Transport Museum Throughout the gallery the muse- set the record on Bonneville, but con- where visitors can design their own Hurtling Fast Notice to Speed um staff worked closely not only with stant rain hampered runs and then futuristic transport and think about Freaks: you may now take a superson- Andy Green but Richard Noble and the salt surface was found to be too how their decisions will shape every- ic ride courtesy of the world’s fastest the ThrustSSC team, to create a slick for the car’s solid aluminum one’s future; Temporary gallery with man, Andy Green, ThrustSSC and the unique land speed record experience alloy wheels causing to handle about regular high profile exhibitions. -
Aerospace Engine Data
AEROSPACE ENGINE DATA Data for some concrete aerospace engines and their craft ................................................................................. 1 Data on rocket-engine types and comparison with large turbofans ................................................................... 1 Data on some large airliner engines ................................................................................................................... 2 Data on other aircraft engines and manufacturers .......................................................................................... 3 In this Appendix common to Aircraft propulsion and Space propulsion, data for thrust, weight, and specific fuel consumption, are presented for some different types of engines (Table 1), with some values of specific impulse and exit speed (Table 2), a plot of Mach number and specific impulse characteristic of different engine types (Fig. 1), and detailed characteristics of some modern turbofan engines, used in large airplanes (Table 3). DATA FOR SOME CONCRETE AEROSPACE ENGINES AND THEIR CRAFT Table 1. Thrust to weight ratio (F/W), for engines and their crafts, at take-off*, specific fuel consumption (TSFC), and initial and final mass of craft (intermediate values appear in [kN] when forces, and in tonnes [t] when masses). Engine Engine TSFC Whole craft Whole craft Whole craft mass, type thrust/weight (g/s)/kN type thrust/weight mini/mfin Trent 900 350/63=5.5 15.5 A380 4×350/5600=0.25 560/330=1.8 cruise 90/63=1.4 cruise 4×90/5000=0.1 CFM56-5A 110/23=4.8 16 -
How It Works Issue 9
NEW THE MAGAZINE THAT FEEDS MINDS INSIDE INTERVIEW DR YAN WONG TM FROM BBC’S BANG SCIENCE ■ ENVIRONMENT ■ TECHNOLOGY ■ TRANSPORT HISTORY ■ SPACE GOES THE THEORY HEART VOLCANIC BYPASSES ERUPTIONS How modern surgeons Discover the explosive save lives everyday BREAK THE 200MB BARRIER! power beneath Earth SUPERFAST BROADBAND LEARN REVEALED! THE NEXT-GENERATION ABOUT NETWORKS THAT DELIVER ■ CASSINI PROBE WARP-SPEED INTERNET ■ RAINING ANIMALS ■ PLANET MERCURY ■ BATTLE OF BRITAIN THE WORLD’S ■ PLACEBO EFFECT ■ LEANING TOWER OF PISA DEADLIEST ■ THE NERVOUS SYSTEM CHOPPER ■ ANDROID VS iPHONE Inside the Apache ■ AVALANCHES 919 AH-64D Longbow FACTS AND 9 ANSWERS 0 INSIDE £3.99 4 0 0 2 3 7 1 4 0 ISSN 2041-7322 2 7 7 ISSUE NINE ISSUE RACE TO 9 HUMAN SOLAR ROLLER 1,000MPH ALLERGIES© Imagine PublishingFLARES Ltd COASTERS Awesome engineering Why dust,No unauthorisedhair and pollen copyingHow massive or distribution explosions on Heart-stopping secrets of behind the land speed record make us sneeze the Sun affect our planet the world’s wildest rides www.howitworksdaily.com 001_HIW_009.indd 1 27/5/10 16:34:18 © Imagine Publishing Ltd No unauthorised copying or distribution Get in touch Have YOU got a question you want answered by the How It Works team? Get in touch by… Email: [email protected] Web: www.howitworksdaily.com ISSUE NINE Snail mail: How It Works Imagine Publishing, 33 Richmond Hill The magazine that feeds minds! Bournemouth, Dorset, BH2 6EZ ”FEED YOUR MIND!” Welcome to How It Meet the experts The sections explained Works issue -
This Is Women's Work
MACHINE MEXICO READY TO FLAT OUT IN REINVENTING WORLD MAKE WAVES BONNEVILLE THE WHEEL Your car is now a better Carlos Slim Domit on The FIA’s Land Speed How Malaysia’s Tony driver than you, so is it putting the heat back Commission hits the home Fernandes plans to change time to hand over the keys? into Formula One of record attempts motoring in Asia INThe international magazineMOTION of the FIA THIS IS WOMEN’S WORK F1 team boss MONISHA KALTENBORN on why modern motor sport no longer has time for sexism PLUS TAXIS RANKED Cab standards under the microscope LATIN LESSONS How Jean Todt’s tour of the Americas raised road safety awareness SHE IS THE LAW Meet F1’s only female race steward STOP UP TO 3 METRES SHORTER WITH MICHELIN ENERGY™ SAVER TYRES.* INSIDE Dear Friends, → INFOCUS 02 Women in motor sport: the general consensus, The latest developments in mobility and motorsport as well as news at least among men, has long been that they were from across the FIA’s worldwide network of clubs not suited to racing, maybe in some predisposed way, ie not strong, or tough enough, to compete with the ‘boys’. Our cover story is a loud and clear refutation of this stereotype. → INSIGHT 14 Through the Women in Motor Sport We report on FIA President Jean Todt’s journey Commission, the FIA is clear in its intent that 12 Latin Lessons through Latin America and how his travels have advanced the cause motor sport is open to all. The women featured in of road safety awareness in the region. -
Gallery of USAF Weapons Note: Inventory Numbers Are Total Active Inventory Figures As of Sept
Gallery of USAF Weapons Note: Inventory numbers are total active inventory figures as of Sept. 30, 2011. ■ 2012 USAF Almanac Bombers B-1 Lancer Brief: A long-range, air refuelable multirole bomber capable of flying intercontinental missions and penetrating enemy defenses with the largest payload of guided and unguided weapons in the Air Force inventory. Function: Long-range conventional bomber. Operator: ACC, AFMC. First Flight: Dec. 23, 1974 (B-1A); Oct. 18, 1984 (B-1B). Delivered: June 1985-May 1988. IOC: Oct. 1, 1986, Dyess AFB, Tex. (B-1B). Production: 104. Inventory: 66. Aircraft Location: Dyess AFB, Tex.; Edwards AFB, Calif.; Eglin AFB, Fla.; Ellsworth AFB, S.D. Contractor: Boeing, AIL Systems, General Electric. Power Plant: four General Electric F101-GE-102 turbofans, each 30,780 lb thrust. Accommodation: pilot, copilot, and two WSOs (offensive and defensive), on zero/zero ACES II ejection seats. Dimensions: span 137 ft (spread forward) to 79 ft (swept aft), length 146 ft, height 34 ft. B-1B Lancer (SSgt. Brian Ferguson) Weight: max T-O 477,000 lb. Ceiling: more than 30,000 ft. carriage, improved onboard computers, improved B-2 Spirit Performance: speed 900+ mph at S-L, range communications. Sniper targeting pod added in Brief: Stealthy, long-range multirole bomber that intercontinental. mid-2008. Receiving Fully Integrated Data Link can deliver nuclear and conventional munitions Armament: three internal weapons bays capable of (FIDL) upgrade to include Link 16 and Joint Range anywhere on the globe. accommodating a wide range of weapons incl up to Extension data link, enabling permanent LOS and Function: Long-range heavy bomber. -
Aircraft Collection
A, AIR & SPA ID SE CE MU REP SEU INT M AIRCRAFT COLLECTION From the Avenger torpedo bomber, a stalwart from Intrepid’s World War II service, to the A-12, the spy plane from the Cold War, this collection reflects some of the GREATEST ACHIEVEMENTS IN MILITARY AVIATION. Photo: Liam Marshall TABLE OF CONTENTS Bombers / Attack Fighters Multirole Helicopters Reconnaissance / Surveillance Trainers OV-101 Enterprise Concorde Aircraft Restoration Hangar Photo: Liam Marshall BOMBERS/ATTACK The basic mission of the aircraft carrier is to project the U.S. Navy’s military strength far beyond our shores. These warships are primarily deployed to deter aggression and protect American strategic interests. Should deterrence fail, the carrier’s bombers and attack aircraft engage in vital operations to support other forces. The collection includes the 1940-designed Grumman TBM Avenger of World War II. Also on display is the Douglas A-1 Skyraider, a true workhorse of the 1950s and ‘60s, as well as the Douglas A-4 Skyhawk and Grumman A-6 Intruder, stalwarts of the Vietnam War. Photo: Collection of the Intrepid Sea, Air & Space Museum GRUMMAN / EASTERNGRUMMAN AIRCRAFT AVENGER TBM-3E GRUMMAN/EASTERN AIRCRAFT TBM-3E AVENGER TORPEDO BOMBER First flown in 1941 and introduced operationally in June 1942, the Avenger became the U.S. Navy’s standard torpedo bomber throughout World War II, with more than 9,836 constructed. Originally built as the TBF by Grumman Aircraft Engineering Corporation, they were affectionately nicknamed “Turkeys” for their somewhat ungainly appearance. Bomber Torpedo In 1943 Grumman was tasked to build the F6F Hellcat fighter for the Navy. -
The Aircraft Propulsion the Aircraft Propulsion
THE AIRCRAFT PROPULSION Aircraft propulsion Contact: Ing. Miroslav Šplíchal, Ph.D. [email protected] Office: A1/0427 Aircraft propulsion Organization of the course Topics of the lectures: 1. History of AE, basic of thermodynamic of heat engines, 2-stroke and 4-stroke cycle 2. Basic parameters of piston engines, types of piston engines 3. Design of piston engines, crank mechanism, 4. Design of piston engines - auxiliary systems of piston engines, 5. Performance characteristics increase performance, propeller. 6. Turbine engines, introduction, input system, centrifugal compressor. 7. Turbine engines - axial compressor, combustion chamber. 8. Turbine engines – turbine, nozzles. 9. Turbine engines - increasing performance, construction of gas turbine engines, 10. Turbine engines - auxiliary systems, fuel-control system. 11. Turboprop engines, gearboxes, performance. 12. Maintenance of turbine engines 13. Ramjet engines and Rocket engines Aircraft propulsion Organization of the course Topics of the seminars: 1. Basic parameters of piston engine + presentation (1-7)- 3.10.2017 2. Parameters of centrifugal flow compressor + presentation(8-14) - 17.10.2017 3. Loading of turbine blade + presentation (15-21)- 31.10.2017 4. Jet engine cycle + presentation (22-28) - 14.11.2017 5. Presentation alternative date Seminar work: Aircraft engines presentation A short PowerPoint presentation, aprox. 10 minutes long. Content of presentation: - a brief history of the engine - the main innovation introduced by engine - engine drawing / cross-section - -
Propulsione Aeronautica 2020/2021 Francesco Barato
PROPULSIONE AERONAUTICA 2020/2021 FRANCESCO BARATO MATERIALE DI SUPPORTO FONDAMENTI DI PROPULSIONE AERONAUTICA Thrust 푇 = (푚̇ 푎 + 푚̇ 푓)푉푒 − 푚̇ 푎푉0 + (푝푒 − 푝푎)퐴푒 푇 ≈ 푚̇ 푎(푉푒 − 푉0) + (푝푒 − 푝푎)퐴푒 1 PROPULSIONE AERONAUTICA 2020/2021 FRANCESCO BARATO Ramjet P-270 Moskit (left), BrahMos (right) Turboramjet Pratt & Whitney J-58 turbo(ram)jet 2 PROPULSIONE AERONAUTICA 2020/2021 FRANCESCO BARATO Scramjet 3 PROPULSIONE AERONAUTICA 2020/2021 FRANCESCO BARATO Specific impulse 푇 푉푒 푇 푚̇ 푝 푉푒 − 푉0 퐼푠푝 = = [푠] 푟표푐푘푒푡푠 퐼푠푝 = = [푠] 푎푟 푏푟푒푎푡ℎ푛푔 푚̇ 푝푔0 푔0 푚̇ 푓푔0 푚̇ 푓 푔0 4 PROPULSIONE AERONAUTICA 2020/2021 FRANCESCO BARATO Propulsive efficiency Overall efficiency Overall efficiency with Mach number 5 PROPULSIONE AERONAUTICA 2020/2021 FRANCESCO BARATO Engine bypass ratios Bypass Engine Name Major applications ratio turbojet early jet aircraft, Concorde 0.0 SNECMA M88 Rafale 0.30 GE F404 F/A-18, T-50, F-117 0.34 PW F100 F-16, F-15 0.36 Eurojet EJ200 Typhoon 0.4 Klimov RD-33 MiG-29, Il-102 0.49 Saturn AL-31 Su-27, Su-30, J-10 0.59 Kuznetsov NK-144A Tu-144 0.6 PW JT8D DC-9, MD-80, 727, 737 Original 0.96 Soloviev D-20P Tu-124 1.0 Kuznetsov NK-321 Tu-160 1.4 GE Honda HF120 HondaJet 2.9 RR Tay Gulfstream IV, F70, F100 3.1 GE CF6-50 A300, DC-10-30,Lockheed C-5M Super Galaxy 4.26 PowerJet SaM146 SSJ 100 4.43 RR RB211-22B TriStar 4.8 PW PW4000-94 A300, A310, Boeing 767, Boeing 747-400 4.85 Progress D-436 Yak-42, Be-200, An-148 4.91 GE CF6-80C2 A300-600, Boeing 747-400, MD-11, A310 4.97-5.31 RR Trent 700 A330 5.0 PW JT9D Boeing 747, Boeing 767, A310, DC-10 5.0 6 PROPULSIONE -
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 .................................... -
Pursuit of Power NASA’S Propulsion Systems Laboratory No
Pursuit of Power NASA’s Propulsion Systems Laboratory No. 1 and 2 By Robert S. Arrighi National Aeronautics and Space Administration NASA History Program Office Public Outreach Division NASA Headquarters Washington, DC 20546 SP–2012–4548 2012 Library of Congress Cataloging-in-Publication Data Arrighi, Robert S., 1969- Pursuit of Power : NASA’s Propulsion Systems Laboratory, No. 1 & 2 / Robert S. Arrighi. p. cm. -- (NASA history series) (NASA SP ; 2012-4548) Includes bibliographical references and index. 1. Propulsion Systems Laboratory (U.S.)--History. 2. Wind tunnels. 3. Hypersonic wind tunnels. 4. Aerodynamics--Research--United States--History--20th century. 5. Propulsion systems--United States--History--20th century. 6. NASA Glenn Research Center. I. United States. NASA History Division. II. Title. III. Title: NASA’s Propulsion Systems Laboratory, No. 1 & 2. IV. Title: Propulsion Systems Laboratory, No. 1 & 2. TL568.P75A77 2012 629.1’1072--dc23 2011032380 • Table of Contents • Introduction ................................................................................................................................................ vii Condensed History of the PSL ......................................................................................................... ix Preserving the PSL Legacy ................................................................................................................. ix Endnotes for Introduction ................................................................................................................. -
Broad Specificationfuels on High B ,Passturbofan Engine Combustors
A/',d_*,,e'/_-/_2 _ Y/ 3 1176 00156 6455 NASA-CR-159641 19790025034 NASA CR-159641 R79AEG504 I,:. Analytical Evaluation of the Impact of " Broad SpecificationFuels on High B_,passTurbofan Engine Combustors FINAL REPORT August 1979 By J. R. Taylor General Electric Company Aircraft Engine Group Cincinnati., OH 45215 Ll_[1_.i[_!_,ll"_l'ti'lit_P7'll_i, ;:t! ,<::iY.ig LANGLEY RE.SEARCH CENTER LIBRARy,NASA HAMPTON,.VIRGINIA . " NATIONAL AERONAUTICS AND SPACEADMINISTRATION LEWISPrepRarEedSEARCHfor: CENTER -: ...... 21000 BROOKPARKROAD CLEVELAND, OHIO 44135 NAS3-20799 1. Report No. I 2. GovernmentA_:cessionNo. 3. Recipient'sCatalogNo. NASA CR-159641 I 4. Title and Subtitle 5. Report Date Analytical Evaluation of the Impact of Broad Specification Fuels August 1979 on High Bypass Turbofan Engine Combustors 6. PerformingOrganizationCode 7. Author{'s) 8. PerformingOrganizationReport No. J.R. Taylor R79AEG504 10. Work Unit No. 9. PerformingOrganizationName andAddress General Electric Company 11. Contractor Grant No. - Aircraft Engine Group Cincinnati, Ohlo 45215 NAS3-20799 13. Type of Report and PeriodCovered 12. SponsoringAgencyName and Address Contractor Report National Aeronautics and Space Administration 14. SponsoringAgency Code Washington, D.C. 20546 15. SupplementaryNotes Project Manager: A.L. Smith, NASA-Lewis Research Center, Cleveland, Ohlo 44135 16.Abstra_ An in-depth analysis of six conceptual combustor designs for the CF6-50 hlgh bypass turbofan engine and slx conceptual combustor designs for the NASA/GE E3 high bypass turbofan engine was performed to provide an assessment of the major problems anticipated in using broad specification fuels in these aircraft engine combustion systems. The conceptual eombustor designs are representative of both state-of-the-art and advanced state-of-the-art combustion systems. -
Why Didn't the Supersonic Car Fly?
Why Didn't The Supersonic KENNETH MORCAN C.Math.FIMA, OUBAY HASSAN AND NICEL WEATHERILL C.Math.FIMA University of Wales Swansea The supersonic car, ThrustSSC, took the World Land Table 1. The World Land Speed Record: major milestones achieved before 1997 Speed Record beyond the speed of sound on the Black Year Driver Nationality Speed Attained (mph) Rock Desert in Nevada in October 1997. To achieve this 1898 Gaston de Ch-Laubat France 39 feat, many challenging technological problems had to be 1904 Louis Rigolly France 103 addressed. One such problem was the aerodynamic de- 1927 Henry Segrave UK 203 sign of the vehicle to ensure that it could be safely oper- 1935 Malcolm Campbell UK 301 1964 Donald Campbell U K 403 ated and, in particular, that it remained in contact with 1964 Craig Breedlove USA 526 the ground at all speeds. Here we outline the role that 1965 Craig Breedlove USA 600 was played by computational fluid dynamics in assisting 1983 Richard Noble U K 633 the process of aerodynamic design. get was 700 mph, but as this was not too far distant from the speed of sound at ground level, which is around 760 mph, he INTRODUCTION decided that he would assemble a team to attempt to take the he first World Land Speed Record was set by Count Record to supersonic speed, ie faster than the speed of sound. Gaston de Chasseloup-Laubat in Acheres, France on Experience had shown, and we'll touch upon this again shortly, TDecember 12 1898. Driving an electric vehicle, he set the that this was not just going to be a matter of making minor mod- Record at 39 mph.