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The Boeing Company 2004 Annual Report the Boeing Company 2004 Annual Report
BC112_Final Cover0302 3/6/05 10:49 PM Page fc1 The Boeing Company The Boeing Company The Boeing Company 2004 Annual Report 100 North Riverside Plaza Chicago, IL 60606-1596 U.S.A. 2004 Annual Report 0707-AR-050707-AR-05 Boeing ifc_ibc_0304 03.04.05 4:06 PM Page ifc1 Vision 2016: People working Shareholder Information The Boeing Company Electronic Proxy Receipt and Voting Duplicate Shareholder Accounts World Headquarters Shareholders have the option of voting their Registered shareholders with duplicate together as a global enterprise The Boeing Company proxies by Internet or telephone, instead of accounts may contact EquiServe for 100 North Riverside Plaza returning their proxy cards through the mail. instructions regarding the consolidation of Chicago, IL 60606-1596 Instructions are in the proxy statement and those accounts. The Company recom- for aerospace leadership. U.S.A. attached to the proxy card for the annual mends that registered shareholders always 312-544-2000 meeting. use the same form of their names in all Registered shareholders can go to stock transactions to be handled in the Strategies Values Transfer Agent, Registrar, Dividend www.econsent.com/ba to sign up to same account. Registered shareholders Run healthy core businesses Leadership Paying Agent and Plan Administrator receive their annual report and proxy state- may also ask EquiServe to eliminate excess The transfer agent is responsible for ment in an electronic format in the future. mailings of annual reports going to share- Leverage strengths into new products and services Integrity shareholder records, issuance of stock, Beneficial owners may contact the brokers holders in the same household. -
Aviation Week & Space Technology
STARTS AFTER PAGE 34 Using AI To Boost How Emirates Is Extending ATM Efficiency Maintenance Intervals ™ $14.95 JANUARY 13-26, 2020 2020 THE YEAR OF SUSTAINABILITY RICH MEDIA EXCLUSIVE 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. -
The Boeing Company 2002 Annual Report
The Boeing Company 200220022002 AnnualAnnualAnnual ReportReportReport Vision 2016: People working together as a global enterprise for aerospace leadership. Strategies Core Competencies Values Run healthy core businesses Detailed customer knowledge Leadership Leverage strengths into new and focus Integrity products and services Large-scale system integration Quality Open new frontiers Lean enterprise Customer satisfaction People working together A diverse and involved team Good corporate citizenship Enhancing shareholder value The Boeing Company Table of Contents Founded in 1916, Boeing evokes vivid images of the amazing products 1 Operational Highlights and services that define aerospace. Each day, more than three million 2 Message to Shareholders passengers board 42,300 flights on Boeing jetliners, more than 345 8 Corporate Essay satellites put into orbit by Boeing launch vehicles pass overhead, and 16 Corporate Governance 6,000 Boeing military aircraft stand guard with air forces of 23 countries 18 Commercial Airplanes and every branch of the U.S. armed forces. 20 Integrated Defense Systems We are the leading aerospace company in the world and a top U.S. 22 Boeing Capital Corporation exporter. We hold more than 6,000 patents, and our capabilities and 24 Air Traffic Management related services include formulation of system-of-systems solutions, 26 Phantom Works advanced information and communications systems, financial services, 28 Connexion by BoeingSM homeland security, defense systems, missiles, rocket engines, launch 30 Shared Services Group systems and satellites. 32 Financials But Boeing is about much more than statistics or products, no matter 88 Selected Products, how awe-inspiring. It’s also about the enterprising spirit of our people Programs and Services working together to provide customers the best solutions possible. -
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October 2006 Volume V, Issue VI www.boeing.com/frontiers LOOKING AHEAD Meet the Advanced Systems organization A SKILLED BUILD 16 of IDS, where Boeing employees are Determinant assembly helps 777 line developing new-technology solutions to support its defense, security, space and THAT FEELS BETTER 28 new market customers A look at Boeing’s wellness resources A QUALITY DECISION 34 Streamlined process aids Boeing, suppliers October 2006 Volume V, Issue VI ON THE COVER: The A160 Hummingbird. Photo by Bob Ferguson O T O BOB FERGUSON PH COVER STORY MOVING AHEAD 12 Employees in the Advanced Systems organization of Integrated Defense Systems—such as those working on the Orbital Express ASTRO demonstration satellite in Huntington Beach, Calif. (above)—are developing future capabilities to support defense, security and other customers. What’s in your wellness toolkit? Boeing offers employees wellness FEELING 28 “tools” from information to services to fitness opportunities. These re- FEATURE sources allow employees to focus on the wellness of themselves and their fam- BETTER ily members. That helps employees be more productive at work and at home. STORY BOEING FRONTIERS October 2006 3 October 2006 Volume V, Issue VI O T O The new 777 Accurate Floor Grid–Determinant T PH Assembly Process gives mechanics easier access R during assembly. It also requires significantly less CKHA 16 O space than the previous three-story tooling struc- L N ture used to build up 777 floor grids. IA R MA COMMERCIAL AIRPLANES INTEGRATED DEFENSE SYSTEMS Parts of a tool What’s the big idea Members of the Manufacturing Engineering team Boeing is developing a high-capacity miniature 16 in Everett, Wash., came up with an idea to improve 20 satellite. -
Arxiv:Math/0209377V2 [Math.NA] 27 Sep 2002 Nsuyn Hserror
Tommy Kunhung Kim September 2001 Applied Mathematics A Modified Smagorinsky Subgrid Scale Model for the Large Eddy Simulation of Turbulent Flow Abstract In the field of Large Eddy Simulation, the Smagorinsky subgrid scale model (in some form) is the most commonly accepted and used subgrid scale model. The purpose of this paper is to address the main weakness of the Smagorinsky model, its poor perfor- mance near the wall. The goal is to establish a model that corrects the Smagorinsky model near the walls while at the same time minimizing the computational over- head. A version the Dynamic Subgrid Scale model is also incorporated into the finite element code to facilitate comparisons with the new model near the walls. One of the unique characteristics of Large Eddy Simulations as compared to other methods of dealing with turbulent flows is the idea of filtering. In this paper we define arXiv:math/0209377v2 [math.NA] 27 Sep 2002 what a filter is and also address an issue related to filters; the error that results when the filtering and differential operations are interchanged. This error is studied under the context of the Finite Element Method which allows us to focus on the function being filtered rather than the filter kernal function, which has been the usual approach in studying this error. A Modified Smagorinsky Subgrid Scale Model for the Large Eddy Simulation of Turbulent Flow BY Tommy Kunhung Kim B.A. (California State University, Fullerton) 1990 M.A. (California State University, Fullerton) 1992 DISSERTATION Submitted in partial satisfaction of the requirements for the degree of DOCTOR OF PHILOSOPHY in Applied Mathematics in the OFFICE OF GRADUATE STUDIES of the UNIVERISTY OF CALIFORNIA arXiv:math/0209377v2 [math.NA] 27 Sep 2002 DAVIS Approved: Committee in Charge 2001 i Abstract In the field of Large Eddy Simulation, the Smagorinsky subgrid scale model (in some form) is the most commonly accepted and used subgrid scale model. -
Optimisation of Aircraft Position in the Formation Flight for the Drag Reduction
Journal of KONES Powertrain and Transport, Vol. 25, No. 3 2018 ISSN: 1231-4005 e-ISSN: 2354-0133 DOI: 10.5604/01.3001.0012.4312 OPTIMISATION OF AIRCRAFT POSITION IN THE FORMATION FLIGHT FOR THE DRAG REDUCTION Adam Antczak, Krzysztof Sibilski Warsaw University of Technology Faculty of Power and Aeronautical Engineering Nowowiejska Street 24, 00-665 Warsaw, Poland e-mail: [email protected], [email protected] Abstract This article presents optimisation of necessary flight thrust in a V-shaped flight formation of small-unmanned plane “Sikorka”. At the beginning is showed analyse of birds behaviour. Their formation flying was the cause of attention in order to minimalize fuel consumption. Afterwards there are overlooked scientific articles about the formation flying subject contain pure physic analyses, and articles about researches which was made in order to explain economic beneficial for airlines. Thus, the article presents mathematical model, which was optimised for three different starting position of a longitudinal axis. After optimisation there are presented results of the wingman position in regard of the leader. Influence of the calculation results on the formation flying was analysed, allowing for some conclusions about the future of the UAV’s flights. The given process is aimed to achieve the best (optimal) solution from the point of view of the specific criterion. The following most important terms can be distinguished within the optimization process: decisive variables – parameters determining the basic project assumptions. The basic design variables and design constrains are described. Keywords: UAV, formation flying, optimisation, dynamic of flight, aerodynamic 1. Introduction In order to engage a client airlines around the world have always been forced not only to offer the highest quality of their services but first of all the most profit able price of a ticket. -
Thermal & Fluid Sciences Industrial Affiliates and Sponsor Conference
Thermal & Fluid Sciences Industrial Affiliates and Sponsor Conference February 1-3, 2017 DAY 1 SESSION I – PSAAP PROGRAM OVERVIEW: Prof. Gianluca Iaccarino Title: Modeling of particle-laden wall turbulence Authors: Mahdi Esmaily, Hoora Abdehkakha Abstract: The study of particle-laden wall turbulence is of prime importance because of its relevance to numerous engineering and scientific applications. We are particularly interested in this problem because of its relevance to characterization and simulation of particle-based solar receivers. The concept behind this new generation of solar receivers is to collect radiative energy volumetrically through dispersed particles rather than the conventional approach of absorption via a surface. In the design under investigation at our center, we explore this concept by seeding nickel particles in a turbulent flow of air in a square duct and exposing the mixture to radiative heat flux. In this setting, particles are heated through radiation, warming the surrounding air that is used for power generation. To make this design practical, the temperature in the near wall region must be maintained below a certain limit. However, due to a phenomenon called turbophoresis, particles interacting with turbulence migrate toward the solid boundaries and produce very high temperatures at the wall by absorbing a significant amount of radiation in a small region. This high local temperature depends primarily on the particle concentration in the viscous sublayer, which its correct prediction relies on proper modeling of turbophoresis. Hence, in this study, we investigate the effect of various parameters on turbophoresis through direct numerical simulations of turbulent flow laden with Lagrangian point-particles. We consider a flow of air in a square duct at a bulk Reynolds number of 5,000 to 20,000 dispersed with 4- to 16-micron nickel particles. -
Curriculum Vitae PROF. ROBERT D. MOSER Department of Theoretical
Curriculum Vitae PROF. ROBERT D. MOSER Department of Theoretical and Applied Mechanics Telephone : (217)-244-7728 University of Illinois at Urbana-Champaign E-mail: [email protected] 104 S. Wright St. Urbana, IL 61801 EDUCATION Ph.D. in Mechanical Engineering, 1984. Stanford University. Dissertation topic: \Direct numerical simulation of curved turbulent channel flow," Adviser: Parviz Moin M.S. in Mechanical Engineering, 1981. Stanford University. B.S. in Mechanical Engineering, 1978. Mass. Institute of Technology. PROFESSIONAL POSITIONS 6/95-Pres. : Professor of Theoretical and Applied Mechanics, University of Illinois, Urbana, IL. 1/02-6/02 : Visiting Professor, Universidad Politechnica de Madrid, Madrid SPAIN. 8/99-8/00 : Interim Head, Department of Theoretical and Applied Mechanics, University of Illinois, Ur- bana, IL. 4/87-6/95 : Research Scientist, NASA Ames Research Center, Moffett Field CA. 4/85-4/87 : Reservoir Engineer, Sohio Petroleum Co., Dallas, TX. 6/84-4/85 : Research Scientist, NASA Ames Research Center, Moffett Field CA. 6/78-6/80 : Analytical Engineer, Hamilton Standard, Windsor Locks CT. RECENT RESEARCH ACTIVITIES Research interests include: 1) Fundamental studies of turbulence using direct numerical simulations. Recent studies have included: investigation of the non-uniqueness and self-similar scaling of turbulent free shear flows, studies of compressibility effects in wall-bounded turbulent flows, investigation of high-Reynolds number scal- ing of wall-bounded turbulence. 2) Development of large eddy simulation (LES) formulations. 3) Development of high resolution numerical methods for use in computational mechanics. 4) Development of high fidelity numerical models of complex multi-scale multi-physics systems. Specific applications include solid propellant rockets, and the cardiovascular system. -
Lecture Notes in Computational Science and Engineering 56
Lecture Notes in Computational Science and Engineering 56 Editors Timothy J. Barth Michael Griebel David E. Keyes Risto M. Nieminen Dirk Roose Tamar Schlick Stavros C. Kassinos Carlos A. Langer Gianluca Iaccarino Parviz Moin (Eds.) Complex Effects in Large Eddy Simulations With 233 Figures, 51 Colour Plates and 17 Tables ABC Editors Stavros C. Kassinos Gianluca Iaccarino Carlos A. Langer Parviz Moin Department of Mechanical Department of Mechanical Engineering and Manufacturing Engineering Stanford University University of Cyprus Escondido Mall 488 Kallipoleos Street 75 94305-3035 Stanford, USA 1678 Nicosia, Cyprus E-mail: [email protected] E-mail: [email protected] [email protected] [email protected] Library of Congress Control Number: 2006933936 Mathematics Subject Classification (2000): 76F65, 80A32, 76F55, 65C20, 76F50, 76M28, 65M15, 65M50 ISBN-10 3-540-34233-8 Springer Berlin Heidelberg New York ISBN-13 978-3-540-34233-5 Springer Berlin Heidelberg New York This work is subject to copyright. All rights are reserved, whether the whole or part of the material is concerned, specifically the rights of translation, reprinting, reuse of illustrations, recitation, broadcasting, reproduction on microfilm or in any other way, and storage in data banks. Duplication of this publication or parts thereof is permitted only under the provisions of the German Copyright Law of September 9, 1965, in its current version, and permission for use must always be obtained from Springer. Violations are liable for prosecution under the German Copyright Law. Springer is a part of Springer Science+Business Media springer.com c Springer-Verlag Berlin Heidelberg 2007 The use of general descriptive names, registered names, trademarks, etc. -
D. J. Bodony 1
D. J. Bodony DANIEL J. BODONY Department of Aerospace Engineering Telephone: 217-244-3844 University of Illinois at Urbana-Champaign, MC-236 http://acoustics.ae.illinois.edu Urbana, IL 61801 E-mail: [email protected] EDUCATION Ph.D., Aeronautics & Astronautics, 2004, Stanford University, Stanford, California. Thesis: Aeroacoustic Prediction of Turbulent Free-Shear Flows M.S., Aeronautics & Astronautics, 1999, Purdue University, West Lafayette, Indiana. Thesis: Turbulence Model Computations of an Axial Vortex. B.S., Aeronautics & Astronautics, 1997, Purdue University, West Lafayette, Indiana. PROFESSIONAL EXPERIENCE Professor August 2020 – Present Department of Aerospace Engineering University of Illinois at Urbana-Champaign, Urbana, Illinois Associate Head and Director of Graduate Studies January 2019 – Present Department of Aerospace Engineering University of Illinois at Urbana-Champaign, Urbana, Illinois Blue Waters Professor January 2014 – Present College of Engineering University of Illinois at Urbana-Champaign, Urbana, Illinois Research Aerospace Engineer and Joint Faculty Fellow October 2018 – Present Vehicle Technology Directorate Army Research Laboratory, Aberdeen Proving Grounds, Aberdeen, Maryland Visiting Professor June 2018 – December 2018 Department of Mechanical Engineering Stanford University, Stanford, California Visiting Professor June 2016 – December 2016 Department of Mechanical Engineering Stanford University, Stanford, California Donald Biggar Willett Faculty Scholar in Engineering April 2016 – Present Department of Aerospace Engineering University of Illinois at Urbana-Champaign, Urbana, Illinois Visiting Professor May 2015 – July 2015 Department of Mechanics KTH Royal Institute of Technology, Stockholm, Sweden Visiting Professor January 2015 – March 2015 Department of Mechanical and Civil Engineering California Institute of Technology, Pasadena, California Associate Professor August 2013 – August 2020 Department of Aerospace Engineering University of Illinois at Urbana-Champaign, Urbana, Illinois 1 D. -
PDF) for the Fatigue Life of the Detail and the Number of Details in the Component (E.G
A REPORT OF THE AIRWORTHINESS ASSURANCE WORKING GROUP RECOMMENDATIONS CONCERNING ARAC TASKING FR Doc. 04-10816 RE: AGING AIRPLANE SAFETY FINAL RULE 14 CFR 121.370a AND 129.16 TASK 3 FINAL REPORT A REPORT OF THE AIRWORTHINESS ASSURANCE WORKING GROUP RECOMMENDATIONS CONCERNING ARAC TASKING FR Doc. 04-10816 RE: AGING AIRPLANE SAFETY FINAL RULE 14 CFR 121.370a AND 129.16 TASK 3 FINAL REPORT FINAL REPORT March 22, 2007 Rev A April 11, 2007 SIGNED BY Rao Varanasi Mark Yerger Co-Chairperson, AAWG Co-Chairperson, AAWG Boeing Commercial Airplanes Federal Express March 22, 2007 Page 1 A REPORT OF THE AIRWORTHINESS ASSURANCE WORKING GROUP RECOMMENDATIONS CONCERNING ARAC TASKING FR Doc. 04-10816 RE: AGING AIRPLANE SAFETY FINAL RULE 14 CFR 121.370a AND 129.16 TASK 3 FINAL REPORT REVISION PAGE LTR DATE CHANGE PAGES PAGES PAGES APPROVED ADDED DELETED CHANGED BY A 11 Apr Page 9, Paragraph A2, Change 9, 11 AWH 07 the word “need” to “should”. Page 11, Repair Recommendation No. 3, Change the phrase “…recommends that repairs for WFD be addressed on a …..” to “….recommends that published repairs be addressed for WFD on a…..” March 22, 2007 Page 2 A REPORT OF THE AIRWORTHINESS ASSURANCE WORKING GROUP RECOMMENDATIONS CONCERNING ARAC TASKING FR Doc. 04-10816 RE: AGING AIRPLANE SAFETY FINAL RULE 14 CFR 121.370a AND 129.16 TASK 3 FINAL REPORT Table of Contents REVISION PAGE..................................................................................................2 Table of Contents..................................................................................................3 -
International Law and Regulation of Aeronautical
INTERNATIONAL LAW AND REGULATION OF AERONAUTICAL PUBLIC CORRESPONDENCE BY SATELLITE The commercial edition of this book is published as volume 3 in the Essential Air and Space Law Series: Tare Brisibe, Aeronautical Public Correspondence by Satellite isbn-10 90-77596-10-0, isbn-13 90-77596-10-4, © Eleven International Publishing This edition is available from Eleven International Publishing P.O. Box 358 3500 AJ Utrecht, The Netherlands Tel.: +31 30 231 0545 Fax: +31 30 225 8045 [email protected] www.elevenpub.com Printed on acid-free paper. ISBN 10: 90-77596-25-9 ISBN 13: 978-90-77596-25-8 © 2006 Tare Brisibe This publication is protected by international copyright law. All rights reserved. No part of this publication may be reproduced, stored in a retrieval system, or transmitted in any form or by any means, electronic, mechanical, photocopying, recording or otherwise, without the prior permission of the publisher. Printed in The Netherlands INTERNATIONAL LAW AND REGULATION OF AERONAUTICAL PUBLIC CORRESPONDENCE BY SATELLITE Proefschrift ter verkrijging van de graad van Doctor aan de Universiteit Leiden, op gezag van de Rector Magnifi cus Dhr Prof.dr. D.D. Breimer, hoogleraar in de faculteit der Wiskunde en Natuurwetenschappen en die der Geneeskunde, volgens besluit van het College van Promoties te verdedigen op donderdag 28 November 2006 te klokke 13.45 uur door Tare Charles Brisibe geboren te Benin, Nigeria in 1968 PROMOTIECOMMISSIE Promotores: Prof. Dr. P. P. C. Haanappel Dr. F. G. von der Dunk Referent: Prof. Dr. F. Lyall (University of Aberdeen) Overige leden:Prof. Dr. E. Back-Impallomeni (University of Padua) Judge G.