Subsystem Architecture Sizing and Analysis for Aircraft Conceptual Design
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Cross & Cockade International SERIALS with PHOTOGRAPHS
Cross & Cockade International THE FIRST WORLD WAR AVIATION HISTORICAL SOCIETY Registered Charity No 1117741 www.crossandcockade.com INDEX for SERIALS with PHOTOGRAPHS This is a provisional index of all the photographs of aircraft with serial numbers in the 46 years of the Cross & Cockade Journal. There are only photographs with identifiable serials, no other items are indexed. Following the Aircraft serial number is the make & model in parentheses, then page number format is: first the volume number, followed by the issue number (1 to 4) between periods with the page number(s) at the end. The cover pages use the last three characters with a 'c' (cover) 'f' - 'r'(front-rear), '1'(outside) '2' (inside). There are over 4180 entries in three categories, British individual aircraft, other countries individual aircraft, followed by airships & balloons. Regretfully, copies of the photographs are not available. Derek Riley, Jan. 22, 2017 AIRCRAFT SERIAL, BRITISH INDIVIDUAL...............................pg 01 AIRCRAFT SERIALS, OTHER COUNTRY...................................pg 13 AIRSHIPS & BALLOONS.............................................................pg 18 AIRCRAFT SERIAL, British individual 81 (Short Folder Seaplane) 07.1.024, 184 (Short Admiralty Type 184) 04.1.cr2, Serial Aircraft type Page num 07.1.027, 15.4.162 06.4.152, 06.4.cf1, 15.4.166, 16.2.064 2 (Short Biplane) 15.4.148 88 (Borel Seaplane) 15.4.167, 16.2.056 187 (Wight Twin Seaplane) 16.2.065 9 (Etrich Taube Monoplane) 15.4.149, 95 (M.Farman Seaplane) 03.4.139, 16.2.057 201 (RAF BE1) 08.4.150, 36.4.256, 42.3.149 46.4.266 97 (H.Farman Biplane) 16.2.057 202 (Bréguet L.2 biplane) 08.4.149 10 (Short Improved S41 Type) 23.4.171, 98 (H.Farman Biplane) 15.4.157 203 (RAF BE3) 08.4.152, 09.4.172, 20.3.134, 34.1.065 103 (Sopwith Tractor Biplane) 15.4.157, 20.3.135, 23.4.169, 28.4.182, 38.4.239, 14 (Bristol Coanda monoplane) 45.3.176 15.4.165 38.4.242, 41.3.162 16 (Avro 503) 15.4.150 104 (Sopwith Tractor Biplane) 03.4.143 204 (RAF BE4) 20.3.134, 23.4.176, 36.1.058 17 (Hydro Recon. -
Airwork Limited
AN APPRECIATION The Council of the Royal Aeronautical Society wish to thank those Companies who, by their generous co-operation, have done so much to help in the production of the Journal ACCLES & POLLOCK LIMITED AIRWORK LIMITED _5£ f» g AIRWORK LIMITED AEROPLANE & MOTOR ALUMINIUM ALVIS LIMITED CASTINGS LTD. ALUMINIUM CASTINGS ^-^rr AIRCRAFT MATERIALS LIMITED ARMSTRONG SIDDELEY MOTORS LTD. STRUCTURAL MATERIALS ARMSTRONG SIDDELEY and COMPONENTS AIRSPEED LIMITED SIR W. G. ARMSTRONG WHITWORTH AIRCRAFT LTD. SIR W. G. ARMSTRONG WHITWORTH AIRCRAFT LIMITED AUSTER AIRCRAFT LIMITED BLACKBURN AIRCRAFT LTD. ^%N AUSTER Blackburn I AIRCRAFT I AUTOMOTIVE PRODUCTS COMPANY LTD. JAMES BOOTH & COMPANY LTD. (H1GH PRECISION! HYDRAULICS a;) I DURALUMIN LJOC kneed *(6>S'f*ir> tttaot • AVIMO LIMITED BOULTON PAUL AIRCRAFT L"TD. OPTICAL - MECHANICAL - ELECTRICAL INSTRUMENTS AERONAUTICAL EQUIPMENT BAKELITE LIMITED BRAKE LININGS LIMITED BAKELITE d> PLASTICS KEGD. TEAM MARKS ilMilNIICI1TIIH I BRAKE AND CLUTCH LININGS T. M. BIRKETT & SONS LTD. THE BRISTOL AEROPLANE CO., LTD. NON-FERROUS CASTINGS AND MACHINED PARTS HANLEY - - STAFFS THE BRITISH ALUMINIUM CO., LTD. BRITISH WIRE PRODUCTS LTD. THE BRITISH AVIATION INSURANCE CO. LTD. BROOM & WADE LTD. iy:i:M.mnr*jy BRITISH AVIATION SERVICES LTD. BRITISH INSULATED CALLENDER'S CABLES LTD. BROWN BROTHERS (AIRCRAFT) LTD. SMS^MMM BRITISH OVERSEAS AIRWAYS CORPORATION BUTLERS LIMITED AUTOMOBILE, AIRCRAFT AND MARITIME LAMPS BOM SEARCHLICHTS AND MOTOR ACCESSORIES BRITISH THOMSON-HOUSTON CO., THE CHLORIDE ELECTRICAL STORAGE CO. LTD. LIMITED (THE) Hxtie AIRCRAFT BATTERIES! Magnetos and Electrical Equipment COOPER & CO. (B'HAM) LTD. DUNFORD & ELLIOTT (SHEFFIELD) LTD. COOPERS I IDBSHU l Bala i IIIIKTI A. C. COSSOR LIMITED DUNLOP RUBBER CO., LTD. -
Approaches to Representing Aircraft Fuel Efficiency Performance for the Purpose of a Commercial Aircraft Certification Standard
APPROACHES TO REPRESENTING AIRCRAFT FUEL EFFICIENCY PERFORMANCE FOR THE PURPOSE OF A COMMERCIAL AIRCRAFT CERTIFICATION STANDARD Brian M. Yutko and R. John Hansman This report is based on the Masters Thesis of Brian M. Yutko submitted to the Department of Aeronautics and Astronautics in partial fulfillment of the requirements for the degree of Master of Science at the Massachusetts Institute of Technology. Report No. ICAT-2011-05 May 2011 MIT International Center for Air Transportation (ICAT) Department of Aeronautics & Astronautics Massachusetts Institute of Technology Cambridge, MA 02139 USA [Page Intentionally Left Blank] -2- Approaches to Representing Aircraft Fuel Efficiency Performance for the Purpose of a Commercial Aircraft Certification Standard by Brian M. Yutko Submitted to the Department of Aeronautics and Astronautics on May 19, 2011 in Partial Fulfillment of the Requirements for the Degree of Master of Science in Aeronautics and Astronautics Abstract Increasing concern over the potential harmful effects of green house gas emissions from various sources has motivated the consideration of an aircraft certification standard as one way to reduce aircraft CO2 emissions and mitigate aviation impacts on the climate. In order to develop a commercial aircraft certification standard, a fuel efficiency performance metric and the condition at which it is evaluated must be determined. The fuel efficiency metric form of interest to this research is fuel/range, where fuel and range can either be evaluated over the course of a reference mission or at a single, instantaneous point. A mission-based metric encompasses all phases of flight and is robust to changes in technology; however, definition of the reference mission requires many assumptions and is cumbersome for both manufacturers and regulators. -
FAA Advisory Circular 20-97B
Subject: AIRCRAFT TIRE MAINTENANCE Date: 4/18/05 AC No.: 20-97B AND OPERATIONAL PRACTICES Initiated by: AFS-306 Change: 1. PURPOSE. This advisory circular (AC) provides recommended tire care and maintenance practices needed to assure the safety of support personnel and the continued airworthiness of aircraft. Specifically, this AC provides guidance on the installation, inflation, maintenance, and removal of aircraft tires. In addition, this AC provides guidance on those operational practices necessary to maintain safe aircraft operations. This AC is not mandatory and does not constitute a regulation. It is issued for guidance purposes and to outline acceptable tire maintenance and operational practices. In lieu of following this method without deviation, operators may elect to follow an alternative method that has also been found acceptable by the Federal Aviation Administration (FAA). 2. CANCELLATION. AC 20-97A, High-Speed Tire Maintenance and Operational Practices, dated May 13, 1987, is cancelled. 3. RELATED REGULATIONS AND DOCUMENTS. a. Title 14 of the Code of Federal Regulations (14 CFR): (1) Part 21, subpart O, Technical Standard Order Authorizations. (2) Part 23, Airworthiness Standards: Normal, Utility, Acrobatic, and Commuter Category Airplanes. (3) Part 25, Airworthiness Standards: Transport Category Airplanes. (4) Part 27, Airworthiness Standards: Normal Category Rotorcraft. (5) Part 29, Airworthiness Standards: Transport Category Rotorcraft. (6) Part 43, Maintenance, Preventive Maintenance, Rebuilding, and Alteration. (7) Part 145, Repair Stations. b. FAA ACs. Copies of the following ACs may be obtained from the U.S. Department of Transportation, Subsequent Distribution Center, Ardmore East Business Center, 3341 Q 75th Avenue, Landover, MD 20785, and may be downloaded at the following Web site: http://www.faa.gov/avr/afs/acs/ac-idx.htm. -
Comparison of Aircraft Tire Wear with Initial Wheel Rotational Speed
International Journal of Aviation, Aeronautics, and Aerospace Volume 2 Issue 1 Article 2 3-2-2015 Comparison of Aircraft Tire Wear with Initial Wheel Rotational Speed Abdurrhman A. Alroqi University of Sussex, [email protected] Weiji Wang University of Sussex, [email protected] Follow this and additional works at: https://commons.erau.edu/ijaaa Part of the Aeronautical Vehicles Commons Scholarly Commons Citation Alroqi, A. A., & Wang, W. (2015). Comparison of Aircraft Tire Wear with Initial Wheel Rotational Speed. International Journal of Aviation, Aeronautics, and Aerospace, 2(1). https://doi.org/10.15394/ ijaaa.2015.1043 This Article is brought to you for free and open access by the Journals at Scholarly Commons. It has been accepted for inclusion in International Journal of Aviation, Aeronautics, and Aerospace by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. Comparison of Aircraft Tire Wear with Initial Wheel Rotational Speed Cover Page Footnote The authors would like to acknowledge University of Sussex for its support with the literature and related resources. This article is available in International Journal of Aviation, Aeronautics, and Aerospace: https://commons.erau.edu/ ijaaa/vol2/iss1/2 Alroqi and Wang: Comparison of Aircraft Tire Wear with Initial Wheel Rotational Speed In this paper, the landing impact of an aircraft is described using a physical model of a single wheel in the main landing gear. The purpose of this study is to understand potential tire-life improvements that could be made by reducing abrasive skidding between aircraft tires and runway surfaces immediately after touchdown. -
2021-03 Pearcey Newby and the Vulcan V2.Pdf
Journal of Aeronautical History Paper 2021/03 Pearcey, Newby, and the Vulcan S C Liddle Vulcan to the Sky Trust ABSTRACT In 1955 flight testing of the prototype Avro Vulcan showed that the aircraft’s buffet boundary was unacceptably close to the design cruise condition. The Vulcan’s status as one of the two definitive carrier aircraft for Britain’s independent nuclear deterrent meant that a strong connection existed between the manufacturer and appropriate governmental research institutions, in this case the Royal Aircraft Establishment (RAE) and the National Physical Laboratory (NPL). A solution was rapidly implemented using an extended and drooped wing leading edge, designed and high-speed wind-tunnel tested by K W Newby of RAE, subsequently being fitted to the scaled test version of the Vulcan, the Avro 707A. Newby’s aerodynamic solution exploited a leading edge supersonic-expansion, isentropic compression* effect that was being investigated at the time by researchers at NPL, including H H Pearcey. The latter would come to be associated with this ‘peaky’ pressure distribution and would later credit the Vulcan implementation as a key validation of the concept, which would soon after be used to improve the cruise efficiency of early British jet transports such as the Trident, VC10, and BAC 1-11. In turn, these concepts were exploited further in the Hawker-Siddeley design for the A300B, ultimately the basis of Britain’s status as the centre of excellence for wing design in Airbus. Abbreviations BS Bristol Siddeley L Lift D Drag M Mach number CL Lift Coefficient NPL National Physical Laboratory Cp Pressure coefficient RAE Royal Aircraft Establishment Cp.te Pressure coefficient at trailing edge RAF Royal Air Force c Chord Re Reynolds number G Load factor t Thickness HS Hawker Siddeley WT Wind tunnel HP Handley Page α Angle of Attack When the airflow past an aerofoil accelerates its pressure and temperature drop, and vice versa. -
Program Schedule
Program Schedule AIAA Science and Technology Forum and Exposition 2015 January 05 - 09, 2015 The Program Report was last updated December 18, 2014 at 04:16 PM EST. To view the most recent meeting schedule online, visit https://aiaa-mst15.abstractcentral.com/planner.jsp Monday, January 05, 2015 Time Session or Event Info 8:00 AM-9:00 AM, Osceola Ballroom CD, PLNRY-01. Opening Keynote , Plenary, Forum 9:00 AM-12:30 PM, St. George 112, ISC-01. International Student Conference (Undergraduate Category), Technical Paper, 53rd AIAA Aerospace Sciences Meeting, Chair: Chris Tavares, The Boeing Company Martian RHOVER Feasibility Study J. Fuentes; R. Pankaja 9:00-9:30 AM Kaluarachchi Satellite Formation Control using Differential Drag S.R. Omar; J.M. 9:30-10:00 AM Wersinger Manufacturing of Triaxial Quasi-three-dimensional Composite 10:00-10:30 AM Materials G. Peterson; D. Liu The Design, Fabrication, and Evaluation of Millimeter Wave Lenses 10:30-11:00 AM for Beamed Energy Applications S.E. Sloan Colorimetric hydrogel-based microfluidic assay system to monitor 11:00-11:30 AM malnutrition in a microgravity environment J.K. Tsosie Significance of Constituent Chemical age on Solid Rocket Propellant 11:30-12:00 PM Regression Rates D.J. Dulin; G.S. Gibson 12:00-12:30 PM Aerodynamic Testing and Development of Sunswift eVe S. Ambrose 9:30 AM-12:30 PM, Miami 2, AA-01. Computational Aeroacoustics I, Technical Paper, 53rd AIAA Aerospace Sciences Meeting, Chair: Walter Eversman, Missouri University of Science and Technology A Computational Study of Flow Within Cavities with Complex 9:30-10:00 AM Geometric Features M.F. -
The Connection
The Connection 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 2011: Royal Air Force Historical Society First published in the UK in 2011 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 978-0-,010120-2-1 Printed by 3indrush 4roup 3indrush House Avenue Two Station 5ane 3itney O72. 273 1 ROYAL AIR FORCE HISTORICAL SOCIETY President 8arshal of the Royal Air Force Sir 8ichael Beetham 4CB CBE DFC AFC Vice-President Air 8arshal Sir Frederick Sowrey KCB CBE AFC Committee Chairman Air Vice-8arshal N B Baldwin CB CBE FRAeS Vice-Chairman 4roup Captain J D Heron OBE Secretary 4roup Captain K J Dearman 8embership Secretary Dr Jack Dunham PhD CPsychol A8RAeS Treasurer J Boyes TD CA 8embers Air Commodore 4 R Pitchfork 8BE BA FRAes 3ing Commander C Cummings *J S Cox Esq BA 8A *AV8 P Dye OBE BSc(Eng) CEng AC4I 8RAeS *4roup Captain A J Byford 8A 8A RAF *3ing Commander C Hunter 88DS RAF Editor A Publications 3ing Commander C 4 Jefford 8BE BA 8anager *Ex Officio 2 CONTENTS THE BE4INNIN4 B THE 3HITE FA8I5C by Sir 4eorge 10 3hite BEFORE AND DURIN4 THE FIRST 3OR5D 3AR by Prof 1D Duncan 4reenman THE BRISTO5 F5CIN4 SCHOO5S by Bill 8organ 2, BRISTO5ES -
Aircraft Tire Data
Aircraft tire Engineering Data Introduction Michelin manufactures a wide variety of sizes and types of tires to the exacting standards of the aircraft industry. The information included in this Data Book has been put together as an engineering and technical reference to support the users of Michelin tires. The data is, to the best of our knowledge, accurate and complete at the time of publication. To be as useful a reference tool as possible, we have chosen to include data on as many industry tire sizes as possible. Particular sizes may not be currently available from Michelin. It is advised that all critical data be verified with your Michelin representative prior to making final tire selections. The data contained herein should be used in conjunction with the various standards ; T&RA1, ETRTO2, MIL-PRF- 50413, AIR 8505 - A4 or with the airframer specifications or military design drawings. For those instances where a contradiction exists between T&RA and ETRTO, the T&RA standard has been referenced. In some cases, a tire is used for both civil and military applications. In most cases they follow the same standard. Where they do not, data for both tires are listed and identified. The aircraft application information provided in the tables is based on the most current information supplied by airframe manufacturers and/or contained in published documents. It is intended for use as general reference only. Your requirements may vary depending on the actual configuration of your aircraft. Accordingly, inquiries regarding specific models of aircraft should be directed to the applicable airframe manufacturer. -
Qtr 02 09 a Quarterly Publication Boeing.Com/Commercial/ Aeromagazine
Qtr_02 09 A QUarterlY PUBLIcatION BOEING.COM/COMMERCIAL/ AEROMAGAZINE Material Management: Providing Customer Solutions 777 Freighter: Greater Efficiency for Long-Haul Operators Landing Gear Program Provides Overhaul Alternative Exceeding Tire Speed Rating During Takeoff Contribution of Flight Systems to Performance-Based Navigation AERO Cover photo: 777 in factory AERO Contents 03 Material Management: Providing Customer Solutions Our services are designed to help airlines operate more efficiently while reducing costs. 05 777 Freighter: Greater Efficiency for Long-Haul Operators The Boeing 777 Freighter is an efficient, long-range, high-capacity freighter offering the advanced features of the 05 777 family. 11 Landing Gear Program Provides Overhaul Alternative Boeing’s overhaul and exchange program offers operators additional options for 11 servicing landing gear. 15 Exceeding Tire Speed Rating During Takeoff Boeing offers guidance to help prevent 15 tire overspeed events during takeoff. 21 Contribution of Flight Systems to Performance-Based Navigation The evolution of flight management systems has led the way for performance- based navigation and the Next Generation 21 Air Transportation System. 01 WWW.boeIng.com/commercIal/aeromagaZIne Issue 34_Quarter 02 | 2009 AERO Publisher Design Cover photography Editorial Board Shannon Frew Methodologie Jeff Corwin Gary Bartz, Frank Billand, Richard Breuhaus, Darrell Hokuf, Al John, Doug Lane, Jill Langer, Mick Pegg, Wade Price, Bob Rakestraw, Editorial director Writer Printer Frank Santoni, Jerome -
Handley Page, Lachmann, Flow Control and Future Civil Aircraft
Handley Page, Lachmann, flow control and future civil aircraft John Green ABSTRACT Frederick Handley Page and Gustav Lachmann independently developed and patented the concept of the slotted wing as a means of increasing maximum lift. Subsequently they co-operated on the project and Lachmann joined Handley Page Ltd. The Handley Page slotted wing became used worldwide, generating substantial income for the company from use of the patent, and its descendents can be found on all modern transport aircraft. In the years following World War II, Lachmann led research at Handley Page to reduce drag by keeping the boundary layer laminar by surface suction. Handley Page led this field in the UK and developed a number of aircraft concepts, none of which came to fruition as full scale projects. However, looking to the future, the basic concept of laminar flow control holds out arguably the greatest potential of all technologies for reducing the fuel burn and environmental impact of future civil aircraft. 1. INTRODUCTION This is the story of two men of genius, Frederick Handley Page and Gustav Lachmann, Figs. 1 and 2. They were brought together by chance, as a result of having independently, and unknown to each other, invented and patented the same aerodynamic concept. During World War I they had been on opposite sides. Handley Page, who had been 28 at the outbreak of hostilities, established his company’s reputation as the designer of the large biplane bombers, the ‘bloody paralysers’ sought by the Royal Navy in 1914, that made a great contribution to the war effort in 1917 and 1918. -
System Requirements Review
AAE 451, SENIOR DESIGN SYSTEM REQUIREMENTS REVIEW TEAM 3: GOLDJET DIANE BARNEY DONALD BARRETT MICHAEL COFFEY JON COUGHLIN MARK GLOVER KEVIN LINCOLN ANDREW MIZENER JARED SCHEID ERIC SMITH Team GoldJet 1 System Requirements Review Table of Contents I. Mission Statement 2 II. Outline of NASA Competition 2 III. Key Assumptions 2 IV. Quality Function Deployment 3 V. Market Research 6 VI. Competitors 11 VII. City Pairs and Key Routes 12 VIII. Design Mission 16 IX. Economic Mission 19 X. Aircraft Sizing 20 XI. Summary and Next Steps 24 XII. References 27 Team GoldJet 2 System Requirements Review I. Mission Statement To design a profitable supersonic aircraft capable of Trans-Pacific travel to meet the needs of airlines and their passengers around the world. II. Outline of NASA Competition The NASA Aeronautics Research Mission Directorate’s (ARMD) 2008-2009 University Competition calls for the design of an N+2 generation supersonic aircraft which would have initial operational capability (IOC) in 2020. More specific goals for the aircraft as outlined by the competition guidelines include: Cruise speed of Mach 1.6 to 1.8 Design Range of 4000 nautical miles Payload of 35-70 passengers, mixed class Fuel Efficiency of 3 passenger-miles per pound of fuel Takeoff field length < 10,000 feet for airport compatibility Supersonic cruise efficiency Low sonic boom (<70 PldB) In addition, entries to the competition are to identify the possible market for a small supersonic airliner, develop design and economic missions for the aircraft (including likely routes), identify technologies that might enable the aircraft design, and complete a conceptual sizing.