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Shelf List 05/31/2011 Matches 4631
Shelf List 05/31/2011 Matches 4631 Call# Title Author Subject 000.1 WARBIRD MUSEUMS OF THE WORLD EDITORS OF AIR COMBAT MAG WAR MUSEUMS OF THE WORLD IN MAGAZINE FORM 000.10 FLEET AIR ARM MUSEUM, THE THE FLEET AIR ARM MUSEUM YEOVIL, ENGLAND 000.11 GUIDE TO OVER 900 AIRCRAFT MUSEUMS USA & BLAUGHER, MICHAEL A. EDITOR GUIDE TO AIRCRAFT MUSEUMS CANADA 24TH EDITION 000.2 Museum and Display Aircraft of the World Muth, Stephen Museums 000.3 AIRCRAFT ENGINES IN MUSEUMS AROUND THE US SMITHSONIAN INSTITUTION LIST OF MUSEUMS THROUGH OUT THE WORLD WORLD AND PLANES IN THEIR COLLECTION OUT OF DATE 000.4 GREAT AIRCRAFT COLLECTIONS OF THE WORLD OGDEN, BOB MUSEUMS 000.5 VETERAN AND VINTAGE AIRCRAFT HUNT, LESLIE LIST OF COLLECTIONS LOCATION AND AIRPLANES IN THE COLLECTIONS SOMEWHAT DATED 000.6 VETERAN AND VINTAGE AIRCRAFT HUNT, LESLIE AVIATION MUSEUMS WORLD WIDE 000.7 NORTH AMERICAN AIRCRAFT MUSEUM GUIDE STONE, RONALD B. LIST AND INFORMATION FOR AVIATION MUSEUMS 000.8 AVIATION AND SPACE MUSEUMS OF AMERICA ALLEN, JON L. LISTS AVATION MUSEUMS IN THE US OUT OF DATE 000.9 MUSEUM AND DISPLAY AIRCRAFT OF THE UNITED ORRISS, BRUCE WM. GUIDE TO US AVIATION MUSEUM SOME STATES GOOD PHOTOS MUSEUMS 001.1L MILESTONES OF AVIATION GREENWOOD, JOHN T. EDITOR SMITHSONIAN AIRCRAFT 001.2.1 NATIONAL AIR AND SPACE MUSEUM, THE BRYAN, C.D.B. NATIONAL AIR AND SPACE MUSEUM COLLECTION 001.2.2 NATIONAL AIR AND SPACE MUSEUM, THE, SECOND BRYAN,C.D.B. MUSEUM AVIATION HISTORY REFERENCE EDITION Page 1 Call# Title Author Subject 001.3 ON MINIATURE WINGS MODEL AIRCRAFT OF THE DIETZ, THOMAS J. -
Communiqué De Presse
Paris, 6th June 2017 PRESS RELEASE First Flight of Russian Aircraft MC-21 Nexeya supplies avionics integration and simulation tools Russia United Aircraft Corporation (UAC) successfully completed the maiden flight of their new MC-21- 300 commercial aircraft at Irkutsk Aviation Plant airfield. Being a modern aircraft, the MC-21 operates with numerous state of the art computer-controlled systems supporting safety-critical flight functions. While this may have been the first time its complex avionics systems have been tested in flight, they have been successfully integrated and tested on the ground thanks to TechSAT’s Avionics Development System ADS2 platform solution. This ADS2 platform enabled UAC Integration Center to test and validate the full MC-21 avionic suits prior to the first flight. Holistic tests including complex operational scenarios were performed during every phases of the design and development of the program ensuring maximum safety and superior performance of the aircraft. TechSAT (a Nexeya company) is proud to be part of the MC-21 program. «TechSAT solutions were designed and built on schedule; all test rigs were thus completed on time», says Victor SINITSYN, head of section at the UAC Integration Center. «ADS2 is a powerful, flexible, and stable product, to perform all required tests. ADS2 keeps its promises. ADS2 functionality is 100% reliable. TechSAT teams are open and skilled to meet customer needs». Marco Häde, TechSAT director of operations : «The key feature of TechSAT’s solutions for MC-21 simulation systems is the integration of all LRUs involved and the cockpit into a real hardware-in-the-loop setup. -
Artifacts and Aircraft
International Journal of Business, Humanities and Technology Vol. 5, No. 2; April 2015 The Ancients: Artifacts and Aircraft Susan Kelly Archer, EdD Embry-Riddle Aeronautical University Department of Doctoral Studies College of Aviation Daytona Beach, Florida USA Abstract Throughout literature and other art forms, certain themes appear repeatedly. The same might be said for engineering designs, specifically the design of aerospace vehicles. In 1996, Lumir Janku wrote about a set of artifacts, discovered in Peru and determined to be Pre-Columbian, that can be interpreted as models of delta- winged fliers. The design of the Peruvian artifacts has been interpreted in multiple ways by a variety of professionals. The delta wing was also incorporated into the design of civilian aircraft during the 20th Century. Modern delta-winged aircraft were used successfully in both military and civilian applications for more than 40 years. It is interesting to read about the possibility that this aeronautical design may have originated millennia earlier with a culture that did not leave written records to explain its artifacts crafted in gold. Keywords: aviation history, delta wing, Pre-Columbian artifacts Throughout literature and other art forms, certain themes appear repeatedly. The same might be said for engineering designs, specifically the design of aerospace vehicles. Man’s fascination with how birds fly can be linked to the ancient legends of Daedalus or the winged Egyptian gods, and then more recently to John Damien’s attempt to fly with wings made from chicken feathers (Brady, 2000) or Otto Lillienthal’s essays linking the physiology of birds to the design of early gliders (Lillienthal, 2001). -
04 Delta Wings
ExperimentalExperimental AerodynamicsAerodynamics Lecture 4: Delta wing experiments G. Dimitriadis Experimental Aerodynamics Introduction •! In this course we will demonstrate the use of several different experimental aerodynamic methodologies •! The particular application will be the aerodynamics of Delta wings at low airspeeds. •! Delta wings are of particular interest because of their lift generation mechanism. Experimental Aerodynamics Delta wing history •! Until the 1930s the vast majority of aircraft featured rectangular, trapezoidal or elliptical wings. •! Delta wings started being studied in the 1930s by Alexander Lippisch in Germany. •! Lippisch wanted to create tail-less aircraft, and Delta wings were one of the solutions he proposed. Experimental Aerodynamics Delta Lippisch DM-1 Designed as an interceptor jet but never produced. The photos show a glider prototype version. Experimental Aerodynamics High speed flight •! After the war, the potential of Delta wings for supersonic flight was recognized both in the US and the USSR. MiG-21 Convair XF-92 Experimental Aerodynamics Low speed performance •! Although Delta wings are designed for high speeds, they still have to take off and land at small airspeeds. •! It is important to determine the aerodynamic forces acting on Delta wings at low speed. •! The lift generated by such wings are low speeds can be split into two contributions: –! Potential flow lift –! Vortex lift Experimental Aerodynamics Delta wing geometry cb Wing surface: S = 2 2b Aspect ratio: AR = "! c c! b AR Sweep angle: tan ! = = 2c 4 b/2! Experimental Aerodynamics Potential flow lift •! Slender wing theory •! The wind is discretized into transverse segments. •! The flow around each segment is modeled as a 2D flow past a flat plate perpendicular to the free stream Experimental Aerodynamics Slender wing theory •! The problem of calculating the flow around the wing becomes equivalent to calculating the flow around each 2D segment. -
CRS Report for Congress Received Through the CRS Web
Order Code RL30730 CRS Report for Congress Received through the CRS Web Russian Fighter Aircraft Industrial Base: Parallels with the United States? November 8, 2000 Christopher Bolkcom Analyst in National Defense Ellen Schwarzler Research Associate Foreign Affairs, Defense, and Trade Division Congressional Research Service The Library of Congress This CRS Report was prepared at the request of Representative James Talent. It has been released for general congressional use with his permission. Russian Fighter Aircraft Industrial Base: Parallels with the United States? Summary There are many differences between the fighter aircraft industry in the United States and in Russia. The United States has traditionally produced its weaponry within a capitalist framework which allowed free enterprise and competition between companies in private industry. The former Soviet Union’s economy, and its fighter aircraft industry was based on a Marxist, command economy, where the central government dictated the type and number of aircraft produced and allocated resources for construction. Once among the most glamorous components of the Soviet military industrial complex, the Russian military aircraft industry has been described by some analysts as being on the verge of collapse. Russia’s civilian aircraft industry has faced similar pressures, which does not bode well for the military aviation infrastructure. It may be difficult for fighter aircraft companies to find employment in Russia’s beleaguered civil aircraft sector. The Russian government has attempted to reform its fighter aircraft industrial base and make it more efficient and competitive with western industry. It has initiated several reforms aimed at reducing the stratification and compartmentalization of industrial processes, as well as improving access to financial resources. -
Future of Vertical Flight
www.vtol.org Kenneth Swartz, Regional Director – Americas The Vertical Flight Society www.vtol.org | [email protected] Kitty Hawk Cora © Vertical Flight Society: CC-BY-SA 4.0 © Vertical Flight Society: CC-BY-SA 4.0 Released March 2018 1 www.vtol.org . Founded as “The American Helicopter Society, Inc.” 75 years ago in Connecticut on Feb. 25, 1943 – “For the purpose of collecting, compiling and disseminating information concerning the helicopter” – Sikorsky Aircraft received its order for the first American helicopters on January 5, 1943 (28 XR-4 helicopters) . The first and longest-serving helicopter non-profit Sikorsky XR-4 helicopter – Founding members Igor Sikorsky, Arthur Young, Frank Piasecki, Courtesy of Sikorsky Aircraft Corp. Stanley Hiller, Reggie Brie, A.A. Griffiths, etc. – Included engineers, pilots, operators and presidents from industry, academia and government in Allied countries . Now 6,000 individual and 95 corporate members . Advancing vertical flight worldwide First Annual AHS Awards Banquet Born with the American Helicopter Industry Oct. 7, 1944 © Vertical Flight Society: CC-BY-SA 4.0 2 www.vtol.org © Vertical Flight Society: CC-BY-SA 4.0 3 www.vtol.org . The international professional society for those working to advance vertical flight – Founded in 1943 as the American Helicopter Society – Everything from VTOL MAVs/UAS to helicopters and eVTOL to STOVL (everything vertical except rockets) CFD of Joby S4, Aug 2015 . Expands knowledge about vertical flight technology and promotes its application around the world . Advances safety and acceptability . Advocates for vertical flight R&D funding . Helps educate and support today’s and tomorrow’s vertical flight engineers and leaders VFF Scholarship Winners at AHS Forum 71, May 2015 © Vertical Flight Society: CC-BY-SA 4.0 4 www.vtol.org . -
The Raf Harrier Story
THE RAF HARRIER STORY ROYAL AIR FORCE HISTORICAL SOCIETY 2 The opinions expressed in this publication are those of the contributors concerned and are not necessarily those held by the Royal Air Force Historical Society. Copyright 2006: Royal Air Force Historical Society First published in the UK in 2006 by the Royal Air Force Historical Society All rights reserved. No part of this book may be reproduced or transmitted in any form or by any means, electronic or mechanical including photocopying, recording or by any information storage and retrieval system, without permission from the Publisher in writing. ISBN 0-9530345-2-6 Printed by Advance Book Printing Unit 9 Northmoor Park Church Road Northmoor OX29 5UH 3 ROYAL AIR FORCE HISTORICAL SOCIETY President Marshal of the Royal Air Force Sir Michael Beetham GCB CBE DFC AFC Vice-President Air Marshal Sir Frederick Sowrey KCB CBE AFC Committee Chairman Air Vice-Marshal N B Baldwin CB CBE FRAeS Vice-Chairman Group Captain J D Heron OBE Secretary Group Captain K J Dearman Membership Secretary Dr Jack Dunham PhD CPsychol AMRAeS Treasurer J Boyes TD CA Members Air Commodore H A Probert MBE MA *J S Cox Esq BA MA *Dr M A Fopp MA FMA FIMgt *Group Captain N Parton BSc (Hons) MA MDA MPhil CEng FRAeS RAF *Wing Commander D Robertson RAF Wing Commander C Cummings Editor & Publications Wing Commander C G Jefford MBE BA Manager *Ex Officio 4 CONTENTS EARLY HISTORICAL PERSPECTIVES AND EMERGING 8 STAFF TARGETS by Air Chf Mshl Sir Patrick Hine JET LIFT by Prof John F Coplin 14 EVOLUTION OF THE PEGASUS VECTORED -
NASA's First A
NASA’s First A Aeronautics from 1958 to 2008 National Aeronautics and Space Administration Office of Communications Public Outreach Division History Program Office Washington, DC 2013 The NASA History Series NASA SP-2012-4412 NASA’s First A Aeronautics from 1958 to 2008 Robert G. Ferguson Library of Congress Cataloging-in-Publication Data Ferguson, Robert G. NASA’s first A : aeronautics from 1958 to 2008 / Robert G. Ferguson. p. cm. -- (The NASA history series) (NASA SP ; 2012-4412) 1. United States. National Aeronautics and Space Administration--History. 2. United States. National Advisory Committee for Aeronautics--History. I. Title. TL521.312.F47 2012 629.130973--dc23 2011029949 This publication is available as a free download at http://www.nasa.gov/ebooks. TABLE OF CONTENTS Acknowledgments vii Chapter 1: The First A: The Other NASA ..................................1 Chapter 2: NACA Research, 1945–58 .................................... 25 Chapter 3: Creating NASA and the Space Race ........................57 Chapter 4: Renovation and Revolution ................................... 93 Chapter 5: Cold War Revival and Ideological Muddle ............141 Chapter 6: The Icarus Decade ............................................... 175 Chapter 7: Caught in Irons ................................................... 203 Chapter 8: Conclusion .......................................................... 229 Appendix: Aeronautics Budget 235 The NASA History Series 241 Index 259 v ACKNOWLEDGMENTS Before naming individuals, I must express my gratitude to those who have labored, and continue to do so, to preserve and share NASA’s history. I came to this project after years of studying private industry, where sources are rare and often inaccessible. By contrast, NASA’s History Program Office and its peers at the laboratories have been toiling for five decades, archiving, cataloging, interviewing, supporting research, and underwriting authors. -
May 1983 Issue of Soaring Magazine
Cambridge Introduces The New M KIV NA V Used by winners at the: 15M French Nationals U.S. 15M Nationals U.S. Open Nationals British Open Nationals Cambridge is pleased to announce the Check These Features: MKIV NAV, the latest addition to the successful M KIV System. Digital Final Glide Computer with • "During Glide" update capability The MKIV NAV, by utilizing the latest Micro • Wind Computation capability computer and LCD technology, combines in • Distance-to-go Readout a single package a Speed Director, a • Altitude required Readout 4-Function Audio, a digital Averager, and an • Thermalling during final glide capability advanced, digital Final Glide Computer. Speed Director with The MKIV NAV is designed to operate with the MKIV Variometer. It will also function • Own LCD "bar-graph" display with a Standard Cambridge Variometer. • No effect on Variometer • No CRUISE/CLIMB switching The MKIV NAV is the single largest invest ment made by Cambridge in state-of-the-art Digital 20 second Averager with own Readout technology and represents our commitment Relative Variometer option to keeping the U.S. in the forefront of soar ing instrumentation. 4·Function Audio Altitude Compensation Cambridge Aero Instruments, Inc. Microcomputer and Custom LCD technology 300 Sweetwater Ave. Bedford, MA 01730 Single, compact package, fits 80mm (31/8") Tel. (617) 275·0889; TWX# 710·326·7588 opening Mastercharge and Visa accepted BUSINESS. MEMBER G !TORGLIDING The JOURNAL of the SOARING SOCIETYof AMERICA Volume 47 • Number 5 • May 1983 6 THE 1983 SSA INTERNATIONAL The Soaring Society of America is a nonprofit SOARING CONVENTION organization of enthusiasts who seek to foster and promote all phases of gliding and soaring on a national and international basis. -
The Development of the Angled-Deck Aircraft Carrier—Innovation And
Naval War College Review Volume 64 Article 5 Number 2 Spring 2011 The evelopmeD nt of the Angled-Deck Aircraft Carrier—Innovation and Adaptation Thomas C. Hone Norman Friedman Mark D. Mandeles Follow this and additional works at: https://digital-commons.usnwc.edu/nwc-review Recommended Citation Hone, Thomas C.; Friedman, Norman; and Mandeles, Mark D. (2011) "The eD velopment of the Angled-Deck Aircraft Carrier—Innovation and Adaptation," Naval War College Review: Vol. 64 : No. 2 , Article 5. Available at: https://digital-commons.usnwc.edu/nwc-review/vol64/iss2/5 This Article is brought to you for free and open access by the Journals at U.S. Naval War College Digital Commons. It has been accepted for inclusion in Naval War College Review by an authorized editor of U.S. Naval War College Digital Commons. For more information, please contact [email protected]. Color profile: Disabled Composite Default screen Hone et al.: The Development of the Angled-Deck Aircraft Carrier—Innovation an THE DEVELOPMENT OF THE ANGLED-DECK AIRCRAFT CARRIER Innovation and Adaptation Thomas C. Hone, Norman Friedman, and Mark D. Mandeles n late 2006, Andrew Marshall, the Director of the Office of Net Assessment in Ithe Office of the Secretary of Defense, asked us to answer several questions: Why had the Royal Navy (RN) developed the angled flight deck, steam catapult, and optical landing aid before the U.S. Navy (USN) did? Why had the USN not devel- oped these innovations, which “transformed carrier Dr. Hone is a professor at the Center for Naval Warfare design and made practical the wholesale use of Studies in the Naval War College, liaison with the Of- fice of the Chief of Naval Operations, and a former se- high-performance jet aircraft,” in parallel with the 1 nior executive in the Office of the Secretary of Defense RN? Once developed by the RN, how had these three and special assistant to the Commander, Naval Air Sys- tems Command. -
Seaplane Design - a Forgotten Art
Verein Deutscher Ingenieure Hamburger Bezirksverein e.V. Arbeitskreis Luft- und Raumfahrt Hamburg Aerospace Lecture Series Hamburger Luft- und Raumfahrtvorträge DGLR in cooperation with the RAeS, HAW Hamburg, VDI, & ZAL invites you to a lecture Seaplane Design - A Forgotten Art Prof. Dr.-Ing. Elmar Wilczek, Expert in Marine Aviation Lecture followed by discussion Date: Thursday, 20 May 2021, 18:00 CEST No registration required ! Online Zoom lecture Online: http://purl.org/ProfScholz/zoom/2021-05-20 Beriev Be-200 Altair – Courtesy of United Aircraft Corporation (UAC) A seaplane gives the ultimate freedom of flight with theoretically endless take-off and alighting possibilities along the coast, on lakes and rivers – and not to forget on the open seas. The design of seaplanes is based on the knowledge of aircraft design and speedboat design. The craft must meet buoyancy and lift requirements. Hydrostatic and -dynamic stability has to be matched with the longitudinal and lateral static and dynamic stability in the air. The structure has to withstand water and air loads. Crucial are hydrodynamic resistance at take-off as well as the lift-to-drag ratio in flight and particularly the water loads in defined sea states. Sea plane design has a glorious past, but much of the knowledge is buried in dusty archives. It is even worse if knowledge is lost forever and needs to be reinvented. Elmar Wilczek has taught seaplane design for decades. In his presentation he will focus on particular research results among others: the importance of water spray for hydrodynamic resistance, scale effects, hydrodynamic elasticity for seaworthiness, length-to-beam ratio for hydrodynamics and aerodynamics. -
Nasa Technical Nasatm X-62,083 Memorandum
1971025733 NASA TECHNICAL NASATM X-62,083 MEMORANDUM O3 00 O < z A FLIGHT EVALUATION OF A VTOL JET TRANSPORT UNDER VISUAL AND SIMULATED INSTRUMENT CONDITIONS Curt A. Holzhauser, Samuel A. Morello, Robert C. Innis, and James M. Fatten Ames Reseach Center Moffett Field, Calif. 94035 Langley Research Center Hampton, Va. 23365 and (ACCESSI R) _._ 1971025733-002 A FLIG}IT EVALUATION OF A VTOL JET TRANSPORT UNDER VISUAL AND SIMULATED INSTRUMENT CONDITIONS By Curt A. Holzhauser*, Samuel A. Morello**, Robert C. Innis *, and James M. Patton** .,."2, *Ames Research Center **Langley Research Center _. '_ ii " ]97]025733-003 TABLE OF CONTENTS SUMMARY Page INTRODUCTION NOTATION ............................ i DESCRIPTION OF AIRPLANE AND EQUIPMENT ............. 5 TEST PROCEDURES AND CONDITIONS ................. ii RESULTS AND DISCUSSION ................... 14 Performance and Basic Operating Procedures ........ ],5 Low speed operational envelope ............ 15 Vertical takeoff and transition ............ 17 Approach and vertical landing ............ 18 Handling qualities .................... 20 Conversion ...................... 21 ILS acquisition and tracking, longitudinal flight path control ..................... 21 Final transition and vertical landing, longitudinal and height control .................. 27 ILS tracking, lateral-directional flight path control . 29 Final transition and vertical landing, lateral control. 31 Trim considerations in transition and hover ...... 36 Terminal area operation ................. 37 Cruise letdown to pro-approach