B-2: the Spirit of Innovation
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Flying Wing Concept for Medium Size Airplane
ICAS 2002 CONGRESS FLYING WING CONCEPT FOR MEDIUM SIZE AIRPLANE Tjoetjoek Eko Pambagjo*, Kazuhiro Nakahashi†, Kisa Matsushima‡ Department of Aeronautics and Space Engineering Tohoku University, Japan Keywords: blended-wing-body, inverse design Abstract The flying wing is regarded as an alternate This paper describes a study on an alternate configuration to reduce drag and structural configuration for medium size airplane. weight. Since flying wing possesses no fuselage Blended-Wing-Body concept, which basically is it may have smaller wetted area than the a flying wing configuration, is applied to conventional airplane. In the conventional airplane for up to 224 passengers. airplane the primary function of the wing is to An aerodynamic design tools system is produce the lift force. In the flying wing proposed to realize such configuration. The configuration the wing has to carry the payload design tools comprise of Takanashi’s inverse and provides the necessary stability and control method, constrained target pressure as well as produce the lift. The fuselage has to specification method and RAPID method. The create lift without much penalty on the drag. At study shows that the combination of those three the same time the fuselage has to keep the cabin design methods works well. size comfortable for passengers. In the past years several flying wings have been designed and flown successfully. The 1 Introduction Horten, Northrop bombers and AVRO are The trend of airplane concept changes among of those examples. However the from time to time. Speed, size and range are application of the flying wing concepts were so among of the design parameters. -
A Clipped Wing: an Assessment of the Effectiveness of the B-21
University of Denver Digital Commons @ DU Electronic Theses and Dissertations Graduate Studies 1-1-2016 A Clipped Wing: An Assessment of the Effectiveness of the B-21 Aidan Thomas Hughes University of Denver Follow this and additional works at: https://digitalcommons.du.edu/etd Part of the International Relations Commons Recommended Citation Hughes, Aidan Thomas, "A Clipped Wing: An Assessment of the Effectiveness of the B-21" (2016). Electronic Theses and Dissertations. 1124. https://digitalcommons.du.edu/etd/1124 This Thesis is brought to you for free and open access by the Graduate Studies at Digital Commons @ DU. It has been accepted for inclusion in Electronic Theses and Dissertations by an authorized administrator of Digital Commons @ DU. For more information, please contact [email protected],[email protected]. A Clipped Wing: An Assessment of the Effectiveness of the B-21 _________________________ A Thesis Presented to the Faculty of the Josef Korbel School of International Studies University of Denver _________________________ In Partial Fulfilment of the Requirements for the Degree Master of Arts _________________________ by Aidan Thomas Hughes June 2016 Advisor: Professor T. Farer Author: Aidan Thomas Hughes Title: A Clipped Wing: An Assessment of the Effectiveness of the B-21 Advisor: Professor T. Farer Degree Date: June 2016 Abstract This thesis examines the effectiveness of the Northrop Grumman B-21 long range strike bomber in advancing the ability of U.S. policy makers to achieve national security objectives. The operational value of the B-21 is assessed through analysing its probable role in four hypothetical combat scenarios, and the relative effectiveness of the B-21 is measured alongside the potential performance of alternative systems. -
Air Force Next-Generation Bomber: Background and Issues for Congress
Air Force Next-Generation Bomber: Background and Issues for Congress Jeremiah Gertler Specialist in Military Aviation December 22, 2009 Congressional Research Service 7-5700 www.crs.gov RL34406 CRS Report for Congress Prepared for Members and Committees of Congress Air Force Next-Generation Bomber: Background and Issues for Congress Summary As part of its proposed FY2010 defense budget, the Administration proposed deferring the start of a program to develop a next-generation bomber (NGB) for the Air Force, pending the completion of the 2010 Quadrennial Defense Review (QDR) and associated Nuclear Posture Review (NPR), and in light of strategic arms control negotiations with Russia. The Administration’s proposed FY2010 budget requested no funding specifically identified in public budget documents as being for an NGB program. Prior to the submission of the FY2010 budget, the Air Force was conducting research and development work aimed at fielding a next-generation bomber by 2018. Although the proposed FY2010 defense budget proposed deferring the start of an NGB program, the Secretary of Defense and Air Force officials in 2009 have expressed support for the need to eventually start such a program. The Air Force’s FY2010 unfunded requirements list (URL)—a list of programs desired by the Air Force but not funded in the Air Force’s proposed FY2010 budget—includes a classified $140-million item that some press accounts have identified as being for continued work on a next-generation bomber. FY2010 defense authorization bill: The conference report (H.Rept. 111-288 of October 7, 2009) on the FY2010 defense authorization act (H.R. -
Aircraft, Defense & Space Domain Business Plan
Aircraft, Defense & Space Domain Business Plan Keisuke Hisakazu Naohiko HIROSE MIZUTANI ABE Senior Vice President, President, Senior Vice President, Head of Commercial Aviation Mitsubishi Aircraft Corporation Head of Integrated Defense Systems & Space Systems June 12, 2017 © 2017 MITSUBISHI HEAVY INDUSTRIES, LTD. All Rights Reserved. Contents 1. Business Overview 2. Commercial Aviation Systems Segment 2-1. Overview 2-2. FY2016 Summary & FY2017 Outlook 2-3. FY2017 Business Strategy 3. MRJ Business 3-1. Overview 3-2. Development Activities 3-3. Implementation of Development Schedule 4. Integrated Defense & Space Systems Segment 4-1. Overview 4-2. FY2016 Summary & FY2017 Outlook 4-3. FY2017 Business Strategy © 2017 MITSUBISHI HEAVY INDUSTRIES, LTD. All Rights Reserved. 1 1-1. Overview (Domain Reorganization) The Aircraft, Defense & Space domain was created as a result of MHI’s domain reorganization, carried out 2017年4月の全社ドメイン再編・事業再配置により、航空・防衛・宇宙ドメインを発足。 in April 2017.直轄による育成基盤の早期形成と収益安定を図る。 Under the CEO’s direct oversight, the new domain is pursuing prompt formation of a strong developmentCEO foundation and stable earnings. [Until March 2017] [From April 2017] Energy & Environment Power Systems Business Group company Mitsubishi Aircraft MRJ Thermal Power Nuclear Power Thermal Power Compressors Corporation Renewable Energy Chemical Plants Aero Engines Nuclear Power Commercial Aviation & Renewable Energy Transportation Systems Commercial / Cruise Land Transportation Ships Systems Industry & Infrastructure Material Handling Commercial Aircraft -
Fly-By-Wire - Wikipedia, the Free Encyclopedia 11-8-20 下午5:33 Fly-By-Wire from Wikipedia, the Free Encyclopedia
Fly-by-wire - Wikipedia, the free encyclopedia 11-8-20 下午5:33 Fly-by-wire From Wikipedia, the free encyclopedia Fly-by-wire (FBW) is a system that replaces the Fly-by-wire conventional manual flight controls of an aircraft with an electronic interface. The movements of flight controls are converted to electronic signals transmitted by wires (hence the fly-by-wire term), and flight control computers determine how to move the actuators at each control surface to provide the ordered response. The fly-by-wire system also allows automatic signals sent by the aircraft's computers to perform functions without the pilot's input, as in systems that automatically help stabilize the aircraft.[1] Contents Green colored flight control wiring of a test aircraft 1 Development 1.1 Basic operation 1.1.1 Command 1.1.2 Automatic Stability Systems 1.2 Safety and redundancy 1.3 Weight saving 1.4 History 2 Analog systems 3 Digital systems 3.1 Applications 3.2 Legislation 3.3 Redundancy 3.4 Airbus/Boeing 4 Engine digital control 5 Further developments 5.1 Fly-by-optics 5.2 Power-by-wire 5.3 Fly-by-wireless 5.4 Intelligent Flight Control System 6 See also 7 References 8 External links Development http://en.wikipedia.org/wiki/Fly-by-wire Page 1 of 9 Fly-by-wire - Wikipedia, the free encyclopedia 11-8-20 下午5:33 Mechanical and hydro-mechanical flight control systems are relatively heavy and require careful routing of flight control cables through the aircraft by systems of pulleys, cranks, tension cables and hydraulic pipes. -
Effects of Aircraft Integration on Compact Nacelle Aerodynamics
Eects of Aircraft Integration on Compact Nacelle Aerodynamics Fernando Tejeroa,∗, Ioannis Goulosa, David G MacManusa, Christopher Sheafb aCentre for Propulsion Engineering, School of Aerospace, Transport and Manufacturing, Craneld University, Bedfordshire, MK43 0AL bRolls-Royce plc., P.O. box 31, Derby, United Kingdom, DE24 8BJ Abstract To reduce specic fuel consumption, it is expected that the next generation of aero-engines will operate with higher bypass-ratios, and therefore fan diame- ters, than current in-service architectures. These new propulsion systems will increase the nacelle size and incur in an additional overall weight and drag con- tribution to the aircraft. In addition, they will be installed more closely-coupled with the airframe, which may lead to an increase in adverse installation eects. As such, it is required to develop compact nacelles which will not counteract the benets obtained from the new engine cycles. A comprehensive investigation of the eects of nacelle design on the overall aircraft aerodynamic performance is required for a better understanding on the eects of aero-engine integration. This paper presents a method for the multi-objective optimisation of drooped and scarfed non-axisymmetric nacelle aero-engines. It uses intuitive Class Shape Tranformations (iCSTs) for the aero-engine geometry denition, multi-point aerodynamic simulation, a near-eld nacelle drag extraction method and the NSGA-II genetic algorithm. The process has been employed for the aerody- namic optimisation of a compact nacelle aero-engine as well as a conventional nacelle conguration. Subsequently, the designed architectures were installed on a conventional commercial transport aircraft and evaluated at dierent in- stallation positions. -
And Octavia Butler's Kindred Across the Sensory Line Emily Anne Bonner University of Tennessee, [email protected]
View metadata, citation and similar papers at core.ac.uk brought to you by CORE provided by University of Tennessee, Knoxville: Trace University of Tennessee, Knoxville Trace: Tennessee Research and Creative Exchange Masters Theses Graduate School 5-2018 Subversive Speculations: Reading Ann Petry's The Street and Octavia Butler's Kindred across the Sensory Line Emily Anne Bonner University of Tennessee, [email protected] Recommended Citation Bonner, Emily Anne, "Subversive Speculations: Reading Ann Petry's The Street and Octavia Butler's Kindred across the Sensory Line. " Master's Thesis, University of Tennessee, 2018. https://trace.tennessee.edu/utk_gradthes/5048 This Thesis is brought to you for free and open access by the Graduate School at Trace: Tennessee Research and Creative Exchange. It has been accepted for inclusion in Masters Theses by an authorized administrator of Trace: Tennessee Research and Creative Exchange. For more information, please contact [email protected]. To the Graduate Council: I am submitting herewith a thesis written by Emily Anne Bonner entitled "Subversive Speculations: Reading Ann Petry's The Street and Octavia Butler's Kindred across the Sensory Line." I have examined the final electronic copy of this thesis for form and content and recommend that it be accepted in partial fulfillment of the requirements for the degree of Master of Arts, with a major in English. Michelle D. Commander, Major Professor We have read this thesis and recommend its acceptance: Thomas F. Haddox, Mary E. Papke Accepted for the -
A52 Mosquito Light Bomber
A52 Mosquito Light Bomber The de Havilland DH 98 Mosquito was one of the greatest combat Initial delays in production were due to the difficulties of importing aircraft of World War II. Originally conceived as a fast, unarmed, light engines, tools and priority equipment from de Havilland in Great Britain bomber that would be able to outfly fighters, the lightweight, all-wood and Canada. Soon after production began, the manufacturer discovered construction “Mossie” first flew on Nov. 25, 1940, and had a top speed an issue with wing assembly, and the first 50 sets of wings required of almost 400 mph. Mosquitoes were built in several different versions, modification. This, and the discovery of flutter issues, further delayed including fighter-bombers (FBs), photo-reconnaissance, day and night production, which eventually amounted to just 75 airplanes being built bombers, and long-range day and night fighters. between March 1944 and May 1945. By the end of the war, production issues had been resolved, and 212 Mosquitoes were built at Bankstown. Mosquitoes were assembled in Great Britain, Canada, and in 1942, the Of these, six FB Mk 40s were converted for photo reconnaissance as Australian de Havilland factory at Bankstown commenced production of PR Mk 40s, and a further 28 were converted to PR Mk 41s, with the last an FB version of the Mosquito. A Royal Air Force Mk II (DD664) was delivered July 22, 1948. delivered to Bankstown and used as a prototype for the Australian FB Mk 40s. It made its first flight on Dec. 17, 1942, and was later delivered In addition to the Australian-built Mosquitoes, 76 British-built Mosquitoes to the Royal Australian Air Force (RAAF) on Jan. -
The Pacific Abhors a Vacuum
January 2014/$5 The Pacifi c Abhors a Vacuum New Tanker Air Force JROTC Aircrew Management January 2014, Vol. 97, No. 1 FEATURES 4 Editorial: Speaking Softly and Carrying a Big Stick By Adam J. Hebert Bombers allow the US to defend its allies without going to war. 20 The Pacifi c Abhors a Vacuum By Marc V. Schanz At AFA’s Pacifi c Air & Space Sympo- sium, top USAF offi cials touted the in- creasing need for engagement across the Asia-Pacifi c region. 26 The Tanker Nears Takeoff By John A. Tirpak After more than a decade of fi ts and stops, USAF’s next tanker is almost here. 32 Finding Luc Gruenther By Peter Grier An F-16 crash was neither the begin- ning nor the end of this story. 42 How Many Aircrew? By Rebecca Grant Rated aircrew management is a constant struggle, with ever-shifting 20 variables. 48 Building the Pilot Force Photography by Jim Haseltine Randolph’s 12th Flying Training Wing keeps the Air Force stocked with ca- pable new pilots. 57 AFJROTC in a Holding Pattern By Peter Grier In recent years, the Air Force-inspired high school citizenship program saw more students, instructors, and units than ever. But plans for growth are fall- ing victim to shrinking budgets. 60 Warbirds By Frederick A. Johnsen Restoring vintage aircraft to like-new condition takes time, money, exper- tise—and lots of TLC. 67 The Feeder Force By John T. Correll Graduates of the Civilian Pilot Training program had a head start toward fl ying About the cover: A B-52H fl ies a training for the AAF in World War II. -
Daniel Egger Papers
http://oac.cdlib.org/findaid/ark:/13030/c87w6jb1 Online items available Daniel Egger papers Finding aid prepared and updated by Gina C Giang. Manuscripts Department The Huntington Library 1151 Oxford Road San Marino, California 91108 Phone: (626) 405-2191 Fax: (626) 449-5720 Email: [email protected] URL: http://www.huntington.org © Finding aid last updated June 2019. The Huntington Library. All rights reserved. Daniel Egger papers mssEgger 1 Descriptive Summary Title: Daniel Egger papers Inclusive Dates: 1927-2019 Collection Number: mssEgger Collector: Egger, Daniel Frederic Extent: 3 boxes, 1 oversize folder, 1 flash drive, and 1 tube (1.04 linear feet) Repository: The Huntington Library, Art Collections, and Botanical Gardens Manuscripts Department 1151 Oxford Road San Marino, California 91108 Phone: (626) 405-2191 Fax: (626) 449-5720 Email: [email protected] URL: http://www.huntington.org Abstract: The Daniel Egger papers include correspondence, printed matter, and photographs related to Daniel Egger’s career in the aerospace industry. Language of Material: The records are in English and Spanish. Access Collection is open to qualified researchers by prior application through the Reader Services Department. For more information, please go to following web site . NOT AVAILABLE: The collection contains one flash drive, which is unavailable until reformatted. Please contact Reader Services for more information. RESTRICTED: Tube 1 (previously housed in Box 1, folder 1). Due to size of original, original will be available only with curatorial permission. Publication Rights The Huntington Library does not require that researchers request permission to quote from or publish images of this material, nor does it charge fees for such activities. -
IIIHIHIIIHIIII O US005143329A United States Patent (19) 11 Patent Number: 5,143,329 Coffinberry (45) Date of Patent: Sep
IIIHIHIIIHIIII O US005143329A United States Patent (19) 11 Patent Number: 5,143,329 Coffinberry (45) Date of Patent: Sep. 1, 1992 (54) GASTURBINE ENGINE POWERED AIRCRAFT ENVIRONMENTAL CONTROL FOREIGN PATENT DOCUMENTS SYSTEM AND BOUNDARY LAYER BLEED 0065855 5/1982 European Pat. Off. (75) Inventor: George A. Coffinberry, West Chester, g 32 E." Ohio 143598 4/1953 United Kingdom. (73) Assignee: General Electric Company, 744923 5/1954 United Kingdom. 774695 4/1955 United Kingdom . Cincinnati, Ohio 846358 6/1958 United Kingdom. 21 Appl. No.: 738,985 1530330 1/1976 United Kingdom . 202.7874 2/1980 United Kingdom ............. 24418.5 22 Filed: Aug. 1, 1991 2074654 4/1980 United Kingdom . 2076897 12/1981 United Kingdom ............. 244/118.5 Related U.S. Application Data 2127492 6/1983 United Kingdom . 62 Division of Ser. No. 531,718, Jun. 1, 1990. Primary Examiner-Joseph F. Peters, Jr. 5 Assistant Examiner-Christopher P. Ellis O2,207. Attorney, Agent, or Firm-Jerome C. Squillaro 244/53 R; 45.4/71 57 ABSTRACT 58) Field of Search ..................... 244/118.5, 207, 208, 244/209 53 R. 60/39. 142 39.07, 39.15, 39.183: An aircraft gas turbine engine is provided with a start s A 4-y 9. '987 ing air turbine that is directly connected through the starter gearbox to the high pressure (HP) shaft and is 56) References Cited provided with an apparatus to extract excess energy U.S. PATENT DOCUMENTS from engine compressor bleed air, return it to the en 2,734,443 2/1956 Wood ..................................... oss gine, and to start the engine with compressed air from 2,777,301 1/1957 Kuhn ..... -
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.