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Author: Frederick Kurt Teichmann
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 458
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Book Description
Author: Frederick Kurt Teichmann
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 458
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Book Description
Author: James A. Quinn
Publisher: CRC Press
ISBN: 9781566767958
Category : Technology & Engineering
Languages : en
Pages : 172
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Book Description
From properties and processes to design and construction analysis, this book collects the information, data and equations that are needed to design simply and economically on a day-to-day basis. Composites: Design Manual presents the information necessary to facilitate the design and procurement of FRP, Graphite and Aramid Composites. It describes mechanical, physical, and environmental properties of composites and materials such as resins, catalysts, reinforcements, multi-axials, and release agents. Over 100 tables, figures, data sheets, and examples simplify the practicalities of composites.
Author: Robert Kyle Schmidt
Publisher: SAE International
ISBN: 0768099420
Category : Technology & Engineering
Languages : en
Pages : 1092
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Book Description
The aircraft landing gear and its associated systems represent a compelling design challenge: simultaneously a system, a structure, and a machine, it supports the aircraft on the ground, absorbs landing and braking energy, permits maneuvering, and retracts to minimize aircraft drag. Yet, as it is not required during flight, it also represents dead weight and significant effort must be made to minimize its total mass. The Design of Aircraft Landing Gear, written by R. Kyle Schmidt, PE (B.A.Sc. - Mechanical Engineering, M.Sc. - Safety and Aircraft Accident Investigation, Chairman of the SAE A-5 Committee on Aircraft Landing Gear), is designed to guide the reader through the key principles of landing system design and to provide additional references when available. Many problems which must be confronted have already been addressed by others in the past, but the information is not known or shared, leading to the observation that there are few new problems, but many new people. The Design of Aircraft Landing Gear is intended to share much of the existing information and provide avenues for further exploration. The design of an aircraft and its associated systems, including the landing system, involves iterative loops as the impact of each modification to a system or component is evaluated against the whole. It is rare to find that the lightest possible landing gear represents the best solution for the aircraft: the lightest landing gear may require attachment structures which don't exist and which would require significant weight and compromise on the part of the airframe structure design. With those requirements and compromises in mind,The Design of Aircraft Landing Gear starts with the study of airfield compatibility, aircraft stability on the ground, the correct choice of tires, followed by discussion of brakes, wheels, and brake control systems. Various landing gear architectures are investigated together with the details of shock absorber designs. Retraction, kinematics, and mechanisms are studied as well as possible actuation approaches. Detailed information on the various hydraulic and electric services commonly found on aircraft, and system elements such as dressings, lighting, and steering are also reviewed. Detail design points, the process of analysis, and a review of the relevant requirements and regulations round out the book content. The Design of Aircraft Landing Gear is a landmark work in the industry, and a must-read for any engineer interested in updating specific skills and students preparing for an exciting career.
Author: Daniel P. Raymer
Publisher: Design Dimentions Press
ISBN: 9780972239707
Category : House & Home
Languages : en
Pages : 143
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Book Description
Easy-to-follow, step-by-step methods to lay out, analyse, and optimise your new homebuilt aircraft concept; Industry methods distilled to the essence, and written in a straight forward, easy-to-read style; No derivations, proofs, or complicated equations. Every step is illustrated with an all-new design example that is followed through from beginning to end.
Author: Mohammad H. Sadraey
Publisher: John Wiley & Sons
ISBN: 1118352807
Category : Technology & Engineering
Languages : en
Pages : 811
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Book Description
A comprehensive approach to the air vehicle design process using the principles of systems engineering Due to the high cost and the risks associated with development, complex aircraft systems have become a prime candidate for the adoption of systems engineering methodologies. This book presents the entire process of aircraft design based on a systems engineering approach from conceptual design phase, through to preliminary design phase and to detail design phase. Presenting in one volume the methodologies behind aircraft design, this book covers the components and the issues affected by design procedures. The basic topics that are essential to the process, such as aerodynamics, flight stability and control, aero-structure, and aircraft performance are reviewed in various chapters where required. Based on these fundamentals and design requirements, the author explains the design process in a holistic manner to emphasise the integration of the individual components into the overall design. Throughout the book the various design options are considered and weighed against each other, to give readers a practical understanding of the process overall. Readers with knowledge of the fundamental concepts of aerodynamics, propulsion, aero-structure, and flight dynamics will find this book ideal to progress towards the next stage in their understanding of the topic. Furthermore, the broad variety of design techniques covered ensures that readers have the freedom and flexibility to satisfy the design requirements when approaching real-world projects. Key features: • Provides full coverage of the design aspects of an air vehicle including: aeronautical concepts, design techniques and design flowcharts • Features end of chapter problems to reinforce the learning process as well as fully solved design examples at component level • Includes fundamental explanations for aeronautical engineering students and practicing engineers • Features a solutions manual to sample questions on the book’s companion website Companion website - www.wiley.com/go/sadraey
Author: Frederick Kurt Teichmann
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 456
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Book Description
Author: International Civil Aviation Organization
Publisher:
ISBN:
Category : Airports
Languages : en
Pages : 172
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Book Description
Author: Federal Aviation Administration
Publisher: Createspace Independent Publishing Platform
ISBN: 9781719061513
Category :
Languages : en
Pages : 348
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Book Description
Airplane Flying Handbook Front Matter Table of Contents Chapter 1: Introduction to Flight Training Chapter 2: Ground Operations Chapter 3: Basic Flight Maneuvers Chapter 4: Maintaining Aircraft Control: Upset Prevention and Recovery Training (PDF) Chapter 5: Takeoffs and Departure Climbs Chapter 6: Ground Reference Maneuvers Chapter 7: Airport Traffic Patterns Chapter 8: Approaches and Landings Chapter 9: Performance Maneuvers Chapter 10: Night Operations Chapter 11: Transition to Complex Airplanes Chapter 12: Transition to Multiengine Airplanes Chapter 13: Transition to Tailwheel Airplanes Chapter 14: Transition to Turbopropeller-Powered Airplanes Chapter 15: Transition to Jet-Powered Airplanes Chapter 16: Transition to Light Sport Airplanes (LSA) Chapter 17: Emergency Procedures Glossary Index
Author: Jack D. Mattingly
Publisher: AIAA
ISBN: 9781600860164
Category : Aircraft gas-turbines
Languages : en
Pages : 732
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Book Description
Annotation A design textbook attempting to bridge the gap between traditional academic textbooks, which emphasize individual concepts and principles; and design handbooks, which provide collections of known solutions. The airbreathing gas turbine engine is the example used to teach principles and methods. The first edition appeared in 1987. The disk contains supplemental material. Annotation c. Book News, Inc., Portland, OR (booknews.com).
Author: Andrew J. Keane
Publisher: John Wiley & Sons
ISBN: 1119406323
Category : Technology & Engineering
Languages : en
Pages : 492
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Book Description
Small Unmanned Fixed-wing Aircraft Design is the essential guide to designing, building and testing fixed wing UAVs (or drones). It deals with aircraft from two to 150 kg in weight and is based on the first-hand experiences of the world renowned UAV team at the UK’s University of Southampton. The book covers both the practical aspects of designing, manufacturing and flight testing and outlines and the essential calculations needed to underpin successful designs. It describes the entire process of UAV design from requirements definition to configuration layout and sizing, through preliminary design and analysis using simple panel codes and spreadsheets to full CFD and FEA models and on to detailed design with parametric CAD tools. Its focus is on modest cost approaches that draw heavily on the latest digital design and manufacturing methods, including a strong emphasis on utilizing off-the-shelf components, low cost analysis, automated geometry modelling and 3D printing. It deliberately avoids a deep theoretical coverage of aerodynamics or structural mechanics; rather it provides a design team with sufficient insights and guidance to get the essentials undertaken more pragmatically. The book contains many all-colour illustrations of the dozens of aircraft built by the authors and their students over the last ten years giving much detailed information on what works best. It is predominantly aimed at under-graduate and MSc level student design and build projects, but will be of interest to anyone engaged in the practical problems of getting quite complex unmanned aircraft flying. It should also appeal to the more sophisticated aero-modeller and those engaged on research based around fixed wing UAVs.
