Introduction To Aircraft Design Second Edition
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Introduction To Aircraft Design
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Author : John P. Fielding
language : en
Publisher: Cambridge University Press
Release Date : 1999-10-14
Introduction To Aircraft Design written by John P. Fielding and has been published by Cambridge University Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 1999-10-14 with Technology & Engineering categories.
"Giving a largely descriptive overview of all aspects of the design process, this well-illustrated account provides an insight into the requirements of each specialist in an aircraft design team. After discussing the need for new designs, the text assesses the merits of different aircraft shapes from micro-lights and helicopters to super-jumbos and V/STOL aircraft."--Back cover.
Introduction To Aircraft Design Second Edition
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Author : John P. Fielding
language : en
Publisher: Cambridge University Press
Release Date : 2017-04-03
Introduction To Aircraft Design Second Edition written by John P. Fielding and has been published by Cambridge University Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 2017-04-03 with Technology & Engineering categories.
This new edition provides a modern, accessible introduction to the whole process of aircraft design together with invaluable data.
General Aviation Aircraft Design
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Author : Snorri Gudmundsson
language : en
Publisher: Butterworth-Heinemann
Release Date : 2013-09-03
General Aviation Aircraft Design written by Snorri Gudmundsson and has been published by Butterworth-Heinemann this book supported file pdf, txt, epub, kindle and other format this book has been release on 2013-09-03 with Technology & Engineering categories.
Find the right answer the first time with this useful handbook of preliminary aircraft design. Written by an engineer with close to 20 years of design experience, General Aviation Aircraft Design: Applied Methods and Procedures provides the practicing engineer with a versatile handbook that serves as the first source for finding answers to realistic aircraft design questions. The book is structured in an "equation/derivation/solved example" format for easy access to content. Readers will find it a valuable guide to topics such as sizing of horizontal and vertical tails to minimize drag, sizing of lifting surfaces to ensure proper dynamic stability, numerical performance methods, and common faults and fixes in aircraft design. In most cases, numerical examples involve actual aircraft specs. Concepts are visually depicted by a number of useful black-and-white figures, photos, and graphs (with full-color images included in the eBook only). Broad and deep in coverage, it is intended for practicing engineers, aerospace engineering students, mathematically astute amateur aircraft designers, and anyone interested in aircraft design. - Organized by articles and structured in an "equation/derivation/solved example" format for easy access to the content you need - Numerical examples involve actual aircraft specs - Contains high-interest topics not found in other texts, including sizing of horizontal and vertical tails to minimize drag, sizing of lifting surfaces to ensure proper dynamic stability, numerical performance methods, and common faults and fixes in aircraft design - Provides a unique safety-oriented design checklist based on industry experience - Discusses advantages and disadvantages of using computational tools during the design process - Features detailed summaries of design options detailing the pros and cons of each aerodynamic solution - Includes three case studies showing applications to business jets, general aviation aircraft, and UAVs - Numerous high-quality graphics clearly illustrate the book's concepts (note: images are full-color in eBook only)
Introduction To Aircraft Aeroelasticity And Loads
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Author : Jan Robert Wright
language : en
Publisher: John Wiley & Sons
Release Date : 2008-02-08
Introduction To Aircraft Aeroelasticity And Loads written by Jan Robert Wright and has been published by John Wiley & Sons this book supported file pdf, txt, epub, kindle and other format this book has been release on 2008-02-08 with Technology & Engineering categories.
Aircraft performance is influenced significantly both by aeroelastic phenomena, arising from the interaction of elastic, inertial and aerodynamic forces, and by load variations resulting from flight and ground manoeuvres and gust / turbulence encounters. There is a strong link between aeroelasticity and loads, and these topics have become increasingly integrated in recent years. Introduction to Aircraft Aeroelasticity and Loads introduces the reader to the main principles involved in a wide range of aeroelasticity and loads topics. Divided into three sections, the book begins by reviewing the underlying disciplines of vibrations, aerodynamics, loads and control. It goes on to describe simplified models to illustrate aeroelastic behaviour and aircraft response before introducing more advanced methodologies. Finally, it explains how industrial certification requirements for aeroelasticity and loads may be met and relates these to the earlier theoretical approaches used. Presents fundamentals of structural dynamics, aerodynamics, static and dynamic aeroelasticity, response and load calculations and testing techniques. Covers performance issues related to aeroelasticity such as flutter, control effectiveness, divergence and redistribution of lift. Includes up-to-date experimental methods and analysis. Accompanied by a website with MatLAB and SIMULINK programs that relate to the models used. Introduction to Aircraft Aeroelasticity and Loads enables the reader to understand the aeroelastic and loads principles and procedures employed in a modern aircraft design office. It will appeal to final year undergraduate and masters students as well as engineers who are new to the aerospace industry.
Introduction To Aeronautics
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Author : Steven A. Brandt
language : en
Publisher: AIAA
Release Date : 2004
Introduction To Aeronautics written by Steven A. Brandt and has been published by AIAA this book supported file pdf, txt, epub, kindle and other format this book has been release on 2004 with Aeronautics categories.
This text and the accompanying AeroDYNAMIC software are designed for use in teaching basic design methods in an introductory course on aeronautics. Brandt (aeronautics, US Air Force Academy) devotes the first chapter of the text to methods of engineering and aircraft design, then covers basic aeronautical engineering methods used in each step of the design process. Final chapters explain how all of the methods are used in the conceptual aircraft design process and present case studies of the development of three well-known aircraft designs. Previous courses in calculus, classical physics, and engineering mechanics are assumed. Annotation : 2004 Book News, Inc., Portland, OR (booknews.com).
Aircraft Engine Design
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Author : Jack D. Mattingly
language : en
Publisher: AIAA
Release Date : 2002
Aircraft Engine Design written by Jack D. Mattingly and has been published by AIAA this book supported file pdf, txt, epub, kindle and other format this book has been release on 2002 with Aircraft gas-turbines categories.
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).
Airworthiness
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Author : Filippo De Florio
language : en
Publisher: Elsevier
Release Date : 2010-12-15
Airworthiness written by Filippo De Florio and has been published by Elsevier this book supported file pdf, txt, epub, kindle and other format this book has been release on 2010-12-15 with Technology & Engineering categories.
Airworthiness: An Introduction to Aircraft Certification, Second Edition, offers a practical guide to the regulations of the International Civil Aviation Organization (ICAO), the U.S. Federal Aviation Administration (FAA), and the European Aviation Safety Agency (EASA). The discussions include the concepts of flight safety and airworthiness; the ICAO and civil aviation authorities; airworthiness requirements; type certifications and the type-certification process; production of products, parts, and appliances; certifications of airworthiness; and rules for "spaceworthiness. The book will be a valuable resource for certification engineers engaged in professional training and practical work in regulatory agencies and aircraft engineering companies. - The only airworthiness guide available—a unique single reference covering the requirements of the ICAO (International Civil Aviation Organisation), FAA (the US Federal Aviation Administration) and EASA (European Aviation Safety Agency) - Demystifies the relevant European and US regulations and helps anyone involved in the manufacture, flying and maintenance of aircraft to understand this complex yet essential topic
Design And Analysis Of Composite Structures
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Author : Christos Kassapoglou
language : en
Publisher: John Wiley & Sons
Release Date : 2011-07-05
Design And Analysis Of Composite Structures written by Christos Kassapoglou and has been published by John Wiley & Sons this book supported file pdf, txt, epub, kindle and other format this book has been release on 2011-07-05 with Technology & Engineering categories.
Design and Analysis of Composite Structures enables graduate students and engineers to generate meaningful and robust designs of complex composite structures. Combining analysis and design methods for structural components, the book begins with simple topics such as skins and stiffeners and progresses through to entire components of fuselages and wings. Starting with basic mathematical derivation followed by simplifications used in real-world design, Design and Analysis of Composite Structures presents the level of accuracy and range of applicability of each method. Examples taken from actual applications are worked out in detail to show how the concepts are applied, solving the same design problem with different methods based on different drivers (e.g. cost or weight) to show how the final configuration changes as the requirements and approach change. Provides a toolkit of analysis and design methods to most situations encountered in practice, as well as analytical frameworks and the means to solving them for tackling less frequent problems. Presents solutions applicable to optimization schemes without having to run finite element models at each iteration, speeding up the design process and allowing examination of several more alternatives than traditional approaches. Includes guidelines showing how decisions based on manufacturing considerations affect weight and how weight optimization may adversely affect the cost. Accompanied by a website at www.wiley.com/go/kassapoglou hosting lecture slides and solutions to the exercises for instructors.
Aircraft Design
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Author : Daniel P. Raymer
language : en
Publisher:
Release Date : 1989
Aircraft Design written by Daniel P. Raymer and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1989 with Technology & Engineering categories.
This textbook for advanced students focuses on industry design practice rather than theoretical definitions. Covers configuration layout, payload considerations, aerodynamics, propulsion, structure and loads, weights, stability, and control, performance, and cost analysis. Annotation copyright Book
Introduction To Aircraft Flight Mechanics
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Author : Thomas R. Yechout
language : en
Publisher: AIAA
Release Date : 2003
Introduction To Aircraft Flight Mechanics written by Thomas R. Yechout and has been published by AIAA this book supported file pdf, txt, epub, kindle and other format this book has been release on 2003 with Aerodynamics categories.
Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.