Concorde 2.0: On-Going Supersonic Projects
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Getting Shipshape
AER October 2020 OSPACE DOES AEROSPACE HAVE A RACE PROBLEM? SECRETS FROM THE FALKLANDS AIR WAR POWERING UP ELECTRIC FLIGHT www.aerosociety.com October 2020 GETTING SHIPSHAPE Volume 47 Number 10 Volume UK F-35B FORCE GETS READY FOR FIRST OPERATIONAL CARRIER DEPLOYMENT Royal AeronauticaSociety OCTOBER 2020 AEROSPACE COVER FINAL.indd 1 18/09/2020 14:59 RAeS 2020 Virtual Conference Programme Join us from wherever you are in the world to experience high quality, informative content. Book early for our special introductory offer rates. STRUCTURES & MATERIALS UAS / ROTORCRAFT / AIR TRANSPORT GREENER BY DESIGN 7th Aircraft Structural Urban Air Mobility RAeS Climate Change Design Conference Conference 2020 Conference 2020 DATE NEW DATE DATE 8 October 22 - 23 October 3 - 4 November TIME TIME TIME 14:00 - 17:00 13:00 - 18:00 13:00 - 18:00 SCAN USING SCAN USING SCAN USING YOUR PHONE YOUR PHONE YOUR PHONE FOR MORE INFO FOR MORE INFO FOR MORE INFO Embark on your virtual learning journey with the RAeS Connect and interact with our speakers and ask questions live Engage and network with other professionals from across the world Meet our sponsors at our virtual exhibitor booths Access content post-event to continue your professional development For the full virtual conference programme and further details on what to expect visit aerosociety.com/VCP Volume 47 Number 10 October 2020 EDITORIAL Contents When global rules unravel Regulars 4 Radome 12 Transmission What price global standards, rules and regulations? Pre-pandemic there were The latest aviation and Your letters, emails, tweets aeronautical intelligence, and social media feedback. -
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. -
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.. -
Supersonic Combustion Ramjet: Analysis on Fuel Options
SUPERSONIC COMBUSTION RAMJET: ANALYSIS ON FUEL OPTIONS by Stephanie W. Barone A thesis submitted to the faculty of The University of Mississippi in partial fulfillment of the requirements of the Sally McDonnell Barksdale Honors College. Oxford May 2004 Approved by ___________________________________ Advisor: Dr. Jeffrey Roux ___________________________________ Reader: Dr. Erik Hurlen ___________________________________ Reader: Dr. John O’Haver 1 © 2016 STEPHANIE BARONE ALL RIGHTS RESERVED 2 ABSTRACT STEPHANIE BARONE: Supersonic Combustion Ramjet: Analysis on Fuel Options This report focuses on different fuel options available to use for scramjet engines. The advantages and disadvantages of JP-7, JP-8, and hydrogen fuels are covered, also the effectiveness and requirements for each fuel are discussed. The recent history of the scramjet engine is included as well as its advantages and disadvantages. An explanation of what each fuel option encompasses and engineering analysis for each fuel are shown. The equations presented for the parametric analysis are shown as functions of the freestream Mach number, with the combustion Mach number as a parameter. The results can be seen for the theoretical possibilities of the scramjet engine and the most likely operating situations. Hydrogen has the highest lower heating value which makes it very appealing to use as a fuel, but it is not very dense so more volume of it is needed to create enough energy. The hydrocarbon fuels, JP-7 and JP-8, have half the value of hydrogen for the lower heating value -
After Concorde, Who Will Manage to Revive Civilian Supersonic Aviation?
After Concorde, who will manage to revive civilian supersonic aviation? By François Sfarti and Sebastien Plessis December 2019 Commercial aircraft are flying at the same speed as 60 years ago. Since Concorde, which made possible to fly from Paris to New York in only 3h30, no civilian airplane has broken the sound barrier. The loudness of the sonic boom was a major technological lock to Concorde success, but 50 years after its first flight, an on-going project led by NASA is about to make supersonic flights over land possible. If successful, it will significantly increase the number of supersonic routes and increase the supersonic aircraft market size substantially. This technological improvement combined with R&D efforts on operational costs and a much larger addressable market than when Concorde flew may revive civilian supersonic aviation in the coming years. Who are the new players at the forefront and the early movers? What are the current investments in this field? What are the key success drivers and remaining technological and regulatory locks to revive supersonic aviation? EXECUTIVE SUMMARY Commercial aircraft are typically flying between 800 km/h and 900 km/h, which is between 75% and 85% of the speed of sound. It is the same speed as 60 years ago and since Concorde, which flew at twice the speed of sound, was retired in 2003, there has been no civilian supersonic aircraft in service. Due to a prohibition to fly supersonic over land and large operational costs, Concorde did not reach commercial success. Even if operational costs would remain larger than subsonic flights, current market environment seems much more favourable: since Concorde was retired in 2003, the air traffic has more than doubled and the willingness to pay can be supported by an increase in the number of high net worth individuals and the fact that business travellers value higher speed levels. -
The Cold War and Beyond
Contents Puge FOREWORD ...................... u 1947-56 ......................... 1 1957-66 ........................ 19 1967-76 ........................ 45 1977-86 ........................ 81 1987-97 ........................ 117 iii Foreword This chronology commemorates the golden anniversary of the establishment of the United States Air Force (USAF) as an independent service. Dedicated to the men and women of the USAF past, present, and future, it records significant events and achievements from 18 September 1947 through 9 April 1997. Since its establishment, the USAF has played a significant role in the events that have shaped modem history. Initially, the reassuring drone of USAF transports announced the aerial lifeline that broke the Berlin blockade, the Cold War’s first test of wills. In the tense decades that followed, the USAF deployed a strategic force of nuclear- capable intercontinental bombers and missiles that deterred open armed conflict between the United States and the Soviet Union. During the Cold War’s deadly flash points, USAF jets roared through the skies of Korea and Southeast Asia, wresting air superiority from their communist opponents and bringing air power to the support of friendly ground forces. In the great global competition for the hearts and minds of the Third World, hundreds of USAF humanitarian missions relieved victims of war, famine, and natural disaster. The Air Force performed similar disaster relief services on the home front. Over Grenada, Panama, and Libya, the USAF participated in key contingency actions that presaged post-Cold War operations. In the aftermath of the Cold War the USAF became deeply involved in constructing a new world order. As the Soviet Union disintegrated, USAF flights succored the populations of the newly independent states. -
Can You Hear the Sonic Boom of a Rocket?
In This Issue Can You Hear The Sonic Boom of a Rocket? Cover Photo: Quest Big Dog rocket kit. Get yours at: www.ApogeeRockets.com/Quest_Big_Dog.asp Apogee Components, Inc. — Your Source For Rocket Supplies That Will Take You To The “Peak-of-Flight” 3355 Fillmore Ridge Heights Colorado Springs, Colorado 80907-9024 USA www.ApogeeRockets.com e-mail: [email protected] ISSUE 265 JULY 13, 2010 Can You Hear The Sonic Boom of A Rocket? By Tim Van Milligan Andrew Metanias asks: “I ordered the Dr. Zooch Saturn V kit a little over a week ago and at the end of the instruc- tions, it said that the rocket goes over 800 feet high and 1144 feet per second on a C6-5. Are they just telling me a bunch of junk to try to make the rocket look cool, or is this really true? 1144 fps is 780 mph. Thats about 20 mph more than the speed of sound (depending on the tempera- ture). It’s hard for me to believe that the detailed Saturn V can break the sound barrier. If anything does go the speed of sound, when it makes a sonic boom and it’s that close by, don’t you have to wear earmuffs or something like that because the sonic boom is extremely loud? Please let me Figure 1: When you push on an incompressible ob- know because I am unsure if I should get a set of C6-5’s for ject, the molecules at the point feel the same push and this kit or not.” move at the same speed as the molecules on the back end. -
46 Reducing Sonic Boom
REDUCING SONIC BOOM - A COLLECTIVE EFFORT STATUS REPORT BY CHARLES ETTER (GULFSTREAM) AND PETER G. COEN (NASA) Several members of the Aviation Industry believe that a new market segment, and possibly a new era of aviation, could be within reach in the next 15 years or less. This new era will reintroduce civil air travel at supersonic speeds. The technical challenges are significant, and progress is being made on many fronts. The economic impact of a new market segment is global, creating new jobs and new technologies. Industry views the development of a socially responsible enroute supersonic noise standard as a parallel effort to technology devel- opment. This new noise standard, in conjunction with relevant environmental standards is beginning to take shape within the ICAO CAEP (Committee for Aviation Environmental Protection) process. The new era of supersonic civil flight could be reintroduced in one of two ways. One way would be to operate at supersonic speed over both water and land, utilizing a low boom aircraft design (unrestricted supersonic flight). The other operational scenario would be to fly at design speeds above Mach 1 over water and unrestricted areas, while slowing down to subsonic speeds, or just over Mach 1, in restricted areas. Flying just over Mach 1.0, between Mach 1.0 and 1.15, is referred to as Mach cut-off. Flying below the Mach cut-off speed will result in the sonic boom waveform not reaching the ground. The actual Mach cut-off speed depends on the prevailing atmospheric conditions. The achievement of commercial supersonic flight will be accomplished via technology breakthroughs developed for smaller aircraft such as business jet aircraft. -
Aviation Week & Space Technology
STARTS AFTER PAGE 34 MRO’s Bumpy Path Rolls Speeds Back to Recovery to Supersonics ™ $14.95 AUGUST 17-30, 2020 ADVANCING AIR MOBILITY Digital Edition Copyright Notice The content contained in this digital edition (“Digital Material”), as well as its selection and arrangement, is owned by Informa. and its affiliated companies, licensors, and suppliers, and is protected by their respective copyright, trademark and other proprietary rights. Upon payment of the subscription price, if applicable, you are hereby authorized to view, download, copy, and print Digital Material solely for your own personal, non-commercial use, provided that by doing any of the foregoing, you acknowledge that (i) you do not and will not acquire any ownership rights of any kind in the Digital Material or any portion thereof, (ii) you must preserve all copyright and other proprietary notices included in any downloaded Digital Material, and (iii) you must comply in all respects with the use restrictions set forth below and in the Informa Privacy Policy and the Informa Terms of Use (the “Use Restrictions”), each of which is hereby incorporated by reference. Any use not in accordance with, and any failure to comply fully with, the Use Restrictions is expressly prohibited by law, and may result in severe civil and criminal penalties. Violators will be prosecuted to the maximum possible extent. You may not modify, publish, license, transmit (including by way of email, facsimile or other electronic means), transfer, sell, reproduce (including by copying or posting on any network computer), create derivative works from, display, store, or in any way exploit, broadcast, disseminate or distribute, in any format or media of any kind, any of the Digital Material, in whole or in part, without the express prior written consent of Informa.