About Supersonic Flight and Mach 3 Flying
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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. -
Best Trade Finance Banking | United States 2019
Financing the Future .InterconnectedWORLD World Is this really reality? AR takes us to the next step Robots... in Turkey Also in this issue... Spring 2019 Start-up funding — venture, angel or IPO? • The business of gaming How green is your juice? • Future-proof career choices • Motoring: Bugatti GBP 9.95 | EUR 14.95 | USD 15.95 BREITLING.COM BREITLING.COM Letter from the editor BOEING has had a terrible start to 2019, commercially and in humanitarian terms, with a crash in Ethiopia claiming the lives of all those aboard one of its 737 Max aircraft. That tragedy came just months after a 737 Max disaster in Indonesia. The delay in grounding the World's Max fleets in the wake of those catastrophic events was the first ethical hiccup; the blanket grounding that should have come immediately was delayed while the American Federal Aviation Administration dallied, and theories were floated about what had, or hadn't, caused the disasters. Unilateral decisions to ground the planes came from individual operators, before regulators or Boeing took a stand. But another, even less defensible, ethical decision had been made by the company, and those carriers purchasing the Max planes, before gaming, and loot. Loot is a lively word, conjuring up any accident had occurred. images of doubloons, pirates and treasure chests, It was revealed, after investigations into the burglars' swags of silverware and pearls, precious safety of the 371 Max aircraft in circulation — things pillaged in war. There are a few lively words post-accidents — that there had been an “optional in that sentence, and while pillage, plunder and extra” warning system for the Max planes. -
Brazilian 14-Xs Hypersonic Unpowered Scramjet Aerospace Vehicle
ISSN 2176-5480 22nd International Congress of Mechanical Engineering (COBEM 2013) November 3-7, 2013, Ribeirão Preto, SP, Brazil Copyright © 2013 by ABCM BRAZILIAN 14-X S HYPERSONIC UNPOWERED SCRAMJET AEROSPACE VEHICLE STRUCTURAL ANALYSIS AT MACH NUMBER 7 Álvaro Francisco Santos Pivetta Universidade do Vale do Paraíba/UNIVAP, Campus Urbanova Av. Shishima Hifumi, no 2911 Urbanova CEP. 12244-000 São José dos Campos, SP - Brasil [email protected] David Romanelli Pinto ETEP Faculdades, Av. Barão do Rio Branco, no 882 Jardim Esplanada CEP. 12.242-800 São José dos Campos, SP, Brasil [email protected] Giannino Ponchio Camillo Instituto de Estudos Avançados/IEAv - Trevo Coronel Aviador José Alberto Albano do Amarante, nº1 Putim CEP. 12.228-001 São José dos Campos, SP - Brasil. [email protected] Felipe Jean da Costa Instituto Tecnológico de Aeronáutica/ITA - Praça Marechal Eduardo Gomes, nº 50 Vila das Acácias CEP. 12.228-900 São José dos Campos, SP - Brasil [email protected] Paulo Gilberto de Paula Toro Instituto de Estudos Avançados/IEAv - Trevo Coronel Aviador José Alberto Albano do Amarante, nº1 Putim CEP. 12.228-001 São José dos Campos, SP - Brasil. [email protected] Abstract. The Brazilian VHA 14-X S is a technological demonstrator of a hypersonic airbreathing propulsion system based on supersonic combustion (scramjet) to fly at Earth’s atmosphere at 30km altitude at Mach number 7, designed at the Prof. Henry T. Nagamatsu Laboratory of Aerothermodynamics and Hypersonics, at the Institute for Advanced Studies. Basically, scramjet is a fully integrated airbreathing aeronautical engine that uses the oblique/conical shock waves generated during the hypersonic flight, to promote compression and deceleration of freestream atmospheric air at the inlet of the scramjet. -
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 -
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 .............................................................. -
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. -
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. -
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. -
Aircraft of Today. Aerospace Education I
DOCUMENT RESUME ED 068 287 SE 014 551 AUTHOR Sayler, D. S. TITLE Aircraft of Today. Aerospace EducationI. INSTITUTION Air Univ.,, Maxwell AFB, Ala. JuniorReserve Office Training Corps. SPONS AGENCY Department of Defense, Washington, D.C. PUB DATE 71 NOTE 179p. EDRS PRICE MF-$0.65 HC-$6.58 DESCRIPTORS *Aerospace Education; *Aerospace Technology; Instruction; National Defense; *PhysicalSciences; *Resource Materials; Supplementary Textbooks; *Textbooks ABSTRACT This textbook gives a brief idea aboutthe modern aircraft used in defense and forcommercial purposes. Aerospace technology in its present form has developedalong certain basic principles of aerodynamic forces. Differentparts in an airplane have different functions to balance theaircraft in air, provide a thrust, and control the general mechanisms.Profusely illustrated descriptions provide a picture of whatkinds of aircraft are used for cargo, passenger travel, bombing, and supersonicflights. Propulsion principles and descriptions of differentkinds of engines are quite helpful. At the end of each chapter,new terminology is listed. The book is not available on the market andis to be used only in the Air Force ROTC program. (PS) SC AEROSPACE EDUCATION I U S DEPARTMENT OF HEALTH. EDUCATION & WELFARE OFFICE OF EDUCATION THIS DOCUMENT HAS BEEN REPRO OUCH) EXACTLY AS RECEIVED FROM THE PERSON OR ORGANIZATION ORIG INATING IT POINTS OF VIEW OR OPIN 'IONS STATED 00 NOT NECESSARILY REPRESENT OFFICIAL OFFICE OF EOU CATION POSITION OR POLICY AIR FORCE JUNIOR ROTC MR,UNIVERS17/14AXWELL MR FORCEBASE, ALABAMA Aerospace Education I Aircraft of Today D. S. Sayler Academic Publications Division 3825th Support Group (Academic) AIR FORCE JUNIOR ROTC AIR UNIVERSITY MAXWELL AIR FORCE BASE, ALABAMA 2 1971 Thispublication has been reviewed and approvedby competent personnel of the preparing command in accordance with current directiveson doctrine, policy, essentiality, propriety, and quality. -
7. Transonic Aerodynamics of Airfoils and Wings
W.H. Mason 7. Transonic Aerodynamics of Airfoils and Wings 7.1 Introduction Transonic flow occurs when there is mixed sub- and supersonic local flow in the same flowfield (typically with freestream Mach numbers from M = 0.6 or 0.7 to 1.2). Usually the supersonic region of the flow is terminated by a shock wave, allowing the flow to slow down to subsonic speeds. This complicates both computations and wind tunnel testing. It also means that there is very little analytic theory available for guidance in designing for transonic flow conditions. Importantly, not only is the outer inviscid portion of the flow governed by nonlinear flow equations, but the nonlinear flow features typically require that viscous effects be included immediately in the flowfield analysis for accurate design and analysis work. Note also that hypersonic vehicles with bow shocks necessarily have a region of subsonic flow behind the shock, so there is an element of transonic flow on those vehicles too. In the days of propeller airplanes the transonic flow limitations on the propeller mostly kept airplanes from flying fast enough to encounter transonic flow over the rest of the airplane. Here the propeller was moving much faster than the airplane, and adverse transonic aerodynamic problems appeared on the prop first, limiting the speed and thus transonic flow problems over the rest of the aircraft. However, WWII fighters could reach transonic speeds in a dive, and major problems often arose. One notable example was the Lockheed P-38 Lightning. Transonic effects prevented the airplane from readily recovering from dives, and during one flight test, Lockheed test pilot Ralph Virden had a fatal accident. -
Effects of Base Shape to Drag at Transonic and Supersonic Speeds by Cfd
DAAAM INTERNATIONAL SCIENTIFIC BOOK 2019 pp. 071-080 Chapter 06 EFFECTS OF BASE SHAPE TO DRAG AT TRANSONIC AND SUPERSONIC SPEEDS BY CFD SERDAREVIC-KADIC, S. & TERZIC, J. Abstract: This work is focused on numerical simulations of air flow around a projectile in order to determine the influence of base shape on the drag coefficient. Simulations are made for transonic and supersonic speeds of air flow. Several shapes of projectile base is considered and the results are compared to drag coefficient of projectile with flat base. Base drag component can be as high as 50% or more of drag and any reduction in base drag can have a large payoff in increased range. Base drag is depended by flow characteristics and geometrical parameters. Influence of base shape to drag coefficient of projectile is studied by commercially CFD code FLUENT. Key words: Drag, Base, Pressure, CFD Authors´ data: Assist. Prof. Dr. Sc. Serdarevic-Kadic S[abina]; Assist. Prof. Dr. Sc. Terzic, J[asmin], Faculty of Mechanical Engineering, University of Sarajevo, Vilsonovo setaliste 9, Sarajevo 71000, Bosnia and Herzegovina, [email protected], [email protected]. This Publication has to be referred as: Serdarevic-Kadic, S[abina] & Terzic, J[asmin] (2019). Effects of Base Shape to Drag at Transonic and Supersonic Speeds by CFD, Chapter 06 in DAAAM International Scientific Book 2019, pp.071-080, B. Katalinic (Ed.), Published by DAAAM International, ISBN 978-3-902734-24-2, ISSN 1726-9687, Vienna, Austria DOI: 10.2507/daaam.scibook.2019.06 071 Serdarevic-Kadic, S. & Terzic, J.: Effects of Base Shape to Drag at Transonic and S.. -
Honda Quits F1! Japanese Manufacturer to Bring Curtain Down on Race-Winning Programme
>> Britain’s Land Speed Record attempt update – see p36 December 2020 • Vol 30 No 12 • www.racecar-engineering.com • UK £5.95 • US $14.50 Honda quits F1! Japanese manufacturer to bring curtain down on race-winning programme CASH CONTROL We reveal the details of Formula 1’s Concorde deal SAFETY CELL The latest in composite chassis technology design INDYCAR SCREEN Aerodine on building US single seater safety device VIRTUAL TRADE Exciting new engineering products for the 2021 season 01 REV30N12_Cover_Honda-ACbs.indd 1 19/10/2020 12:56 THE EVOLUTION IN FLUID HORSEPOWER ™ ™ XRP® ProPLUS RaceHose and ™ XRP® Race Crimp Hose Ends A full PTFE smooth-bore hose, manufactured using a patented process that creates convolutions only on the outside of the tube wall, where they belong for increased flexibility, not on the inside where they can impede flow. This smooth-bore race hose and crimp-on hose end system is sized to compete directly with convoluted hose on both inside diameter and weight while allowing for a tighter bend radius and greater flow per size. Ten sizes from -4 PLUS through -20. Additional "PLUS" sizes allow for even larger inside hose diameters as an option. CRIMP COLLARS Two styles allow XRP NEW XRP RACE CRIMP HOSE ENDS™ Race Crimp Hose Ends™ to be used on the ProPLUS Black is “in” and it is our standard color; Race Hose™, Stainless braided CPE race hose, XR- Blue and Super Nickel are options. Hundreds of styles are available. 31 Black Nylon braided CPE hose and some Bent tube fixed, double O-Ring sealed swivels and ORB ends.