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Concorde Is a Museum Piece, but the Allure of Speed Could Spell Success
CIVIL SUPERSONIC Concorde is a museum piece, but the allure Aerion continues to be the most enduring player, of speed could spell success for one or more and the company’s AS2 design now has three of these projects. engines (originally two), the involvement of Air- bus and an agreement (loose and non-exclusive, by Nigel Moll but signed) with GE Aviation to explore the supply Fourteen years have passed since British Airways of those engines. Spike Aerospace expects to fly a and Air France retired their 13 Concordes, and for subsonic scale model of the design for the S-512 the first time in the history of human flight, air trav- Mach 1.5 business jet this summer, to explore low- elers have had to settle for flying more slowly than speed handling, followed by a manned two-thirds- they used to. But now, more so than at any time scale supersonic demonstrator “one-and-a-half to since Concorde’s thunderous Olympus afterburn- two years from now.” Boom Technology is working ing turbojets fell silent, there are multiple indi- on a 55-seat Mach 2.2 airliner that it plans also to cations of a supersonic revival, and the activity offer as a private SSBJ. NASA and Lockheed Martin appears to be more advanced in the field of busi- are encouraged by their research into reducing the ness jets than in the airliner sector. severity of sonic booms on the surface of the planet. www.ainonline.com © 2017 AIN Publications. All Rights Reserved. For Reprints go to Shaping the boom create what is called an N-wave sonic boom: if The sonic boom produced by a supersonic air- you plot the pressure distribution that you mea- craft has long shaped regulations that prohibit sure on the ground, it looks like the letter N. -
Ovrhyp, Scramjet Test Aircraft STATE UNIVERSITY Student Authors: J
https://ntrs.nasa.gov/search.jsp?R=19910000728 2020-03-19T20:21:21+00:00Z /z7 H OVRhyp, Scramjet Test Aircraft STATE UNIVERSITY Student Authors: J. Asian, T. Bisard, S. Dallinga, K. Draper, G. Hufford, W. Peters, and J. Rogers Supervisor: Dr. G. M. Gregorek Assistant: R. L. Reuss Department of Aeronautical & Astronautical Engineering Universities Space Research Association Houston, Texas 77058 Subcontract Dated November 17, 1989 Final Report May 1990 03/0_ OVRhyp, Scramjet Test Aircraft UNIVERSITY Student Authors: J. Asian, T. Bisard, S. Dallinga, K. Draper, G. Hufford, W. Peters, and J. Rogers Supervisor: Dr. G. M. Gregorek Assistant: R. L. Reuss Department of Aeronautical & Astronautical Engineering Universities Space Research Association Houston, Texas 77058 Subcontract Dated November 17, 1989 Final Report RF Project 767919/722941 May 1990 ABSTRACT (Gary Huff0rd} A preliminary design for an unmanned hypersonic research vehicle to test scramjet engines is presented. The aircraft will be launched from a carrier aircraft at an altitude of 4Q,0QQ feet at Mach 0.8. The vehicle will then accelerate to Mach 6 at an altitude of 100,000 feet. At this stage the prototype scramjet will be employed to accelerate the vehicle to Mach 10 and maintain Mach IQ flight for 2 minutes. The aircraft will then decelerate and safely land, presumably at NASA Dryden F[i_ht Test Center. ii TABLE OF CONTENTS ABSTRACT ............................ ii TABLE OF CONTENTS ....................... iii LIST OF FIGURES ......................... v INTRODUCTION .......................... vi CONFIGURATION .......................... WEIGHTS ANALYSIS ........................ 12 PURPOSE ............................. 12 METHOD ........................... 12 SYSTEMS .......................... 14 AERODYNAMIC SURFACES .................... 14 BODY STRUCTURE ....................... 15 THERMAL PROTECTION SYSTEM ................. 15 LAUNCH AND LANDING SYSTEM ................ -
Aviation Week & Space Technology
$14.95 JUNE 29-JULY 12, 2020 Quest for Speed BOOM XB-1 TAKES SHAPE RICH MEDIA EXCLUSIVE Europe’s Hydrogen- Powered Aircraft Push PRIME TIME FOR How Safe Are HYPERSONICS Aircraft Cabins? Canada’s Fighter RICH MEDIA EXCLUSIVE Strategy 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. -
Aviation Week & Space Technology
STARTS AFTER PAGE 34 How Air Trvel New Momentum for My Return Smll Nrrowbodies? ™ $14.95 APRIL 20-MAY 3, 2020 SUSTAINABLY 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. -
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. -
Aerospace and Aviation
GE Aviation in Evendale, Ohio. Where Aerospace and Aviation Companies Take Flight Ohio’s Innovative and Collaborative Environment Ohio is the birthplace of aviation and continues today as a place for leading-edge aerospace research, innovation and collaborative development. As the No. 1 supplier state to Boeing and Airbus, Ohio is a powerhouse producer of systems and parts for the aerospace industry, leveraging our innovation infrastructure and our manufacturing know- how. In addition, our mix of government, corporate and military investment in the industry make Ohio the ideal location for companies looking to expand and advance their aviation and aerospace operations. COTSWORKS in Highland Heights, Ohio. A Highly Skilled and Continuously Expanding Aerospace and Aviation Workforce Ohio’s skilled workforce, talent pipeline, training programs and higher education institutions provide aerospace and aviation companies the skilled workers they need to take their innovations to new heights. rd Largest Manufacturing 3 Workforce in the U.S. 18,000+ Engineering and Science degrees Graduate Each Year From 38,000+ 80+ University Campuses in the State Employees in the Private Aerospace Industry SEVEN Colleges and Universities Conducting th Highest Number UAS and Advanced Technology Research 5 of Top Aerospace Jobs in the Nation The National UAS Training and Certification Center located at Sinclair Community College Aerospace and 550+ Aviation Firms Innovation in the Sky and Beyond With $12 billion in R&D investments, Ohio is home to hundreds of organizations dedicated to advancing aerospace and aviation breakthroughs. Companies in Ohio can collaborate with government, academic, military, industry peers and industry organizations to develop and commercialize their latest aerospace and aviation technology. -
Vysoké Učení Technické V Brně Zavedení a Provoz Supersonického Business Jetu
VYSOKÉ UÈENÍ TECHNICKÉ V BRNĚ BRNO UNIVERSITY OF TECHNOLOGY FAKULTA STROJNÍHO INŽENÝRSTVÍ LETECKÝ ÚSTAV FACULTY OF MECHANICAL ENGINEERING INSTITUTE OF AEROSPACE ENGINEERING ZAVEDENÍ A PROVOZ SUPERSONICKÉHO BUSINESS JETU LAUNCHING AND OPERATING ISSUES OF SUPERSONIC BUSINESS JET DIPLOMOVÁ PRÁCE MASTER'S THESIS AUTOR PRÁCE Bc. DANIELA KINCOVÁ AUTHOR VEDOUCÍ PRÁCE Ing. RÓBERT ©O©OVIÈKA, Ph.D. SUPERVISOR BRNO 2015 Abstrakt Tato práce se zabývá problematikou zavedení a provozu nadzvukových business jetù. V dnešní době se v civilní letecké pøepravě, po ukončení provozu Concordu, žádná nadzvuková letadla nevyskytují. V dnešní době existuje mnoho projektù a organizací, které se zabý- vají znovuzavedením nadzvukových letounù do civilního letectví a soustředí se pøevážně na business jety. Hlavní otázkou je, zda je vùbec vhodné, èi rozumné se k tomu typu dopravy znovu vracet. Existuje hodně problémù, které toto komplikují. Tyto letouny způsobují příliš velký hluk, mají obrovskou spotøebu paliva a musí øe¹it nadměrné emise, létají ve vysokých výškách ve kterých mùže docházet k problémùm s pøetlakováním kabiny, navi- gací, radioaktivním zářením apod. Navíc zákaz supersonických letù nad pevninou letové cesty omezuje a prodlužuje. Současně vznikající projekty navíc nedosahují tak velkého doletu jako klasické moderní bussjety, což zpùsobuje, že se nadzvukové business jety se na delších tratích stávají neefektivní. I pøes tyto problémy, je víceméně jisté, že k zavedení nadzvukových business jetù dojde během následujících 10 - 15 let, i kdyby to měla být jen otázka jisté prestiže velmi bohatých lidí. Summary This thesis is dealing with problematic about launching and operating supersonic business jets. Nowadays, after Concorde retirement, there are no more any supersonic aircrafts in civil transport system. -
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. -
Congress and the Supersonic Transport, 1960-1971 by John
Congress and the supersonic transport, 1960-1971 by John Marion Bell A thesis submitted in partial fulfillment of the requirements for the degree of MASTER OF ARTS in History Montana State University © Copyright by John Marion Bell (1974) Abstract: Aviation state-of-the-art advances in the 1940's and 1950's paved the way for development of a commercial SST in the 1960's. Military aviation advances were translated directly into subsonic transports and it was felt that the next step in progress would be the SST. Through military programs and basic research by NACA, the United States government aided the development of a commercial SST even before undertaking an active SST program in the 1960's. Foreign governments were also at work on SST's and when the British and French merged their development programs in 1962 the United States was spurred by their competition. President Kennedy announced an active program in June, 1963 a day following Pan Am's order of Anglo-French SST's. There was little opposition to the airplane at first; what little there was was based on the aircraft's unavoidable sonic boom. A design competition was conducted by the FAA to select the best possible American design. Boeing was selected the winner in 1966 on the basis of a radical, swing-wing design. The program then entered a two-prototype development stage. Boeing soon ran into development problems and in 1968 abandoned its swing-wing in favor of a conventional fixed-wing. The airplane's problems were also complicated by the great increase in cost of development as well as a growing opposition based on the possible negative environmental impact of the SST. -
On the Ballistic Wave from Projectiles and Vehicles of Simple Geometry Jean Varnier, Marie-Claire Le Pape, Frédéric Sourgen
On the ballistic wave from projectiles and vehicles of simple geometry Jean Varnier, Marie-Claire Le Pape, Frédéric Sourgen To cite this version: Jean Varnier, Marie-Claire Le Pape, Frédéric Sourgen. On the ballistic wave from projectiles and vehicles of simple geometry. AIAA Journal, American Institute of Aeronautics and Astronautics, 2018, 56 (7), pp.2725-2742. 10.2514/1.J056239. hal-01852518 HAL Id: hal-01852518 https://hal.archives-ouvertes.fr/hal-01852518 Submitted on 1 Aug 2018 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. On the ballistic wave from projectiles and vehicles of simple geometry Jean Varnier*, Marie-Claire Le Pape° ONERA, 92320 Châtillon, France Frédéric Sourgen°° ONERA, 31400 Toulouse, France The ballistic wave is a shock wave generated by a solid body moving at supersonic speed in the atmosphere. It sounds like the crack of a whip for small projectiles, like a detonation (sonic boom) for large-sized objects. Their common signature is a N-shaped pressure profile, the formalism of which is well-known but presents a practical difficulty, namely the calculation of the “shape factor” which characterizes the aerodynamic behavior of the object flying at supersonic speed. -
Examining Explanations for the Strange Phenomena Encountered by U.S
AIRCRAFT DESIGN 14 LUNAR SPACESUITS 18 SUPERSONICS 36 Perlan 2 glider — explained More fl exibility for astronauts Listening for X-59’s sonic thump Mystery sightings Examining explanations for the strange phenomena encountered by U.S. Navy pilots. PAGE 26 NOVEMBER 2019 | A publication of the American Institute of Aeronautics and Astronautics | aerospaceamerica.aiaa.org The Premier Global, Commercial, Civil, Military and Emergent Space Conference Where Ideas Launch • Connections Are Made • Business Gets Done! SpaceSymposium.org SAVE $600 – Register Today for Best Savings! Special Military Rates! +1.800.691.4000 Share: FEATURES | November 2019 MORE AT aerospaceamerica.aiaa.org The Premier Global, Commercial, Civil, Military and Emergent Space Conference 14 18 36 26 Aiming for Exploring the Planning for 90,000 feet moon in new the sound of Mystery phenomena spacesuits Designers of Perlan 2 supersonic fl ight We look at possible explanations for those overcame formidable Former astronaut How NASA’s Low Boom fast and agile objects zipping across F/A-18 engineering Tom Jones examines Flight Demonstrator screens. challenges to NASA’s plans to give will test the public’s create a glider that explorers suits that tolerance for sonic By Jan Tegler and Cat Hofacker has reached the will let them walk, thumps. stratosphere and will lope, crouch and even try to beat its own kneel. By Jan Tegler record next year. Where Ideas Launch • Connections Are Made • Business Gets Done! By Tom Jones By Keith Button SpaceSymposium.org SAVE $600 – Register Today for -
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 .................................................................................................