Make America Boom Again: How to Bring Back Supersonic Transport Eli Dourado and Samuel Hammond
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
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. -
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 -
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. -
Feeling Supersonic
FlightGlobal.com May 2021 How Max cuts hurt Boeing backlog Making throwaway Feeling aircraft aff ordable p32 Hydrogen switch for Fresson’s Islander p34 supersonic Will Overture be in tune with demand? p52 9 770015 371327 £4.99 Big worries Warning sign We assess A380 Why NOTAM outlook as last burden can delivery looms baffl e pilots 05 p14 p22 Comment Prospects receding Future dreaming Once thought of as the future of air travel, the A380 is already heading into retirement, but aviation is keenly focused on the next big thing Airbus t has been a rapid rise and fall for on who you ask. As we report else- Hydrogen is not without its the Airbus A380, which not so where in this issue, there are those issues, of course, but nonethe- long ago was being hailed as the banking on supersonic speeds be- less it appears more feasible as a future of long-haul air travel. ing the answer. power source for large transport IThe superjumbo would be, The likes of Aerion and Boom Su- aircraft than batteries do at pres- forecasts said, the perfect tool for personic view the ability to shave ent, even allowing for improving airlines operating into mega-hubs significant time from journeys as a energy densities. such as Dubai that were beginning unique selling point. However, there are others who to spring up. While projects are likely to be see hydrogen through a differ- But the planners at Airbus failed technologically feasible, to be able ent filter. They argue that so- to take into consideration the to sell these new aircraft in signif- called sub-regional aircraft – the efficiency gains available from icant volumes their manufacturers Britten-Norman Islander, among a new generation of widebody will have to ensure that supersonic others – can be given fresh impetus twinjets that allowed operators to flight is not merely the domain of if a fuel source can be found that is open up previously uneconomical the ultra-rich. -
HISTORICAL PERSPECTIVE a Need for Speed
n HISTORICAL PERSPECTIVE A need for speed Mach 0.8 to 1.2 and above the speed of powerful turbine engine available. To mit- Skystreak taught lots sound, respectively). The U.S. Army Air igate as much risk as possible, the team Forces took responsibility for supersonic kept the design simple, using a conven- about flight near research—which resulted in Chuck Yea- tional straight wing rather than the new ger breaking the sound barrier in the Bell and mostly unproven swept wing. The the sound barrier X-1 on Oct. 14, 1947. That historic event 5,000-lb.-thrust (22-kilonewton) Allison overshadowed the highly successful re- J35-A-11 engine filled the fuselage, leav- BY MICHAEL LOmbARDI search conducted by the pilots who flew ing just enough room to house instrumen- s World War II was coming to a the Douglas D-558-1 Skystreak to the edge tation and a pilot in a cramped cockpit. close, advances in high-speed aero- of the sound barrier while capturing new Because of the lack of knowledge about Adynamics were rapidly progressing world speed records. the survivability of a high-altitude, high- beyond the ability of the wind tunnels of The D-558-1 was developed by the speed bailout, Douglas engineers designed the day, prompting a dramatic expansion Douglas Aircraft Company, today a part a jettisonable nose section that could pro- of flight-test research and experimental of Boeing, at its El Segundo (Calif.) tect the pilot until a safe bailout speed was aircraft. Division. It was designed by a team led reached. -
CHAPTER 11 Subsonic and Supersonic Aircraft Emissions
CHAPTER 11 Subsonic and Supersonic Aircraft Emissions Lead Authors: A. Wahner M.A. Geller Co-authors: F. Arnold W.H. Brune D.A. Cariolle A.R. Douglass C. Johnson D.H. Lister J.A. Pyle R. Ramaroson D. Rind F. Rohrer U. Schumann A.M. Thompson CHAPTER 11 SUBSONIC AND SUPERSONIC AIRCRAFT EMISSIONS Contents SCIENTIFIC SUMMARY ......................................................................................................................................... 11.1 11.1 INTRODUCTION ............................................................................................................................................ 11.3 11.2 AIRCRAFT EMISSIONS ................................................................................................................................. 11.4 11.2.1 Subsonic Aircraft .................................................................................................................................. 11.5 11.2.2 Supersonic Aircraft ............................................................................................................................... 11.6 11.2.3 Military Aircraft .................................................................................................................................... 11.6 11.2.4 Emissions at Altitude ............................................................................................................................ 11.6 11.2.5 Scenarios and Emissions Data Bases ................................................................................................... -
Diffusion Flames and Supersonic Combustion
DIFFUSION FLAMES AND SUPERSONIC COMBUSTION BY I.DA-RIVA A.LINAN E. FRAGA J. L. URRUTI A INSTITUTO NACIONAL DE TECNICA AEROESPACIAL «ESTEBAN TERRA DAS» MADRID (SPAIN) October i, 1566 ABSTRACT The paper describes some analytical work connected with the purely diffusive mode of supersonic combustion. The basic problems considered have been: the study of the hydrogen-air diffusion flames, under hoth close to and far from equilibrium conditions, and the study of the aerodynamic field near the injector exit when the ratio of injected to outer total pressures is small. The internal structure of hydrogen-oxygen diffusion flames close to equilibrium has been studied using the first order approximation of an asymptotic expansion method, in which the large parameter represents the ratio between a characteris tic mechanical time and a chemical time. Far from equilibrium conditions, the above mentioned solution fails. However, when a free jet of hydrogen.parallel to the air stream is used for injection purposes, a very simple near frozen approach may be used. The main simplifying features of such an approach being; the use of an overall chemical reaction, the assumption that fuel and oxidizer jnix without appreciable depletion and chemical heat release, and the linearization of the mixing problem. Finally a discussion of some means of improving the mixing process, near the injector exit, is made, using some experimental evidence from work on related problems by other groups. TABLE OF CONTENTS Pa INTRODUCTION 1 1 HYDROGEN AIR DIFFUSION FLAME CLOSE TO EQUILIBRIUM . 3 1A Structure of the Diffusion Flames 4 IB Hydrogen-Oxygen Chemical Kinetics 7 IC Structure of the Hydrogen-Air Diffusion Flames. -
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. -
Make America Boom Again: How to Bring Back Supersonic Transport,” Eli Dourado and Samuel Hammond Show That It Is Time to Revisit the Ban
MAKE AMERICA BOOM AGAIN How to Bring Back Supersonic Transport _____________________ In 1973, the Federal Aviation Administration (FAA) banned civil supersonic flight over the United States, stymieing the development of a supersonic aviation industry. In “Make America Boom Again: How to Bring Back Supersonic Transport,” Eli Dourado and Samuel Hammond show that it is time to revisit the ban. Better technology—including better materials, engines, and simulation capabilities—mean it is now possible to produce a supersonic jet that is more economical and less noisy than those of the 1970s. It is time to rescind the ban in favor of a more modest and sensible noise standard. BACKGROUND Past studies addressing the ban on supersonic flight have had little effect. However, this paper takes a comprehensive view of the topic, covering the history of supersonic flight, the case for supersonic travel, the problems raised by supersonic flight, and regulatory alternatives to the ban. Dourado and Hammond synthesize the best arguments for rescinding the ban on supersonic flights over land and establish that the ban has had a real impact on the development of supersonic transport. KEY FINDINGS The FAA Should Replace the Ban on Overland Supersonic Flight with a Noise Standard The sonic boom generated by the Concorde and other early supersonic aircraft was very loud, and as a result the FAA banned flights in the United States from going faster than the speed of sound (Mach 1). This ban should be rescinded and replaced with a noise standard. A noise limit of 85–90 A-weighted decibels would be similar to noise standards for lawnmowers, blenders, and motorcy- cles, and would therefore be a reasonable standard during daytime hours.