Introduction to Aircraft Flight Mechanics PDF Download
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Author: Thomas R. Yechout Publisher: AIAA ISBN: 9781600860782 Category : Aerodynamics Languages : en Pages : 666
Book Description
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.
Author: Thomas R. Yechout Publisher: AIAA ISBN: 9781600860782 Category : Aerodynamics Languages : en Pages : 666
Book Description
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.
Author: John P. Fielding Publisher: Cambridge University Press ISBN: 1107393353 Category : Technology & Engineering Languages : en Pages : 290
Book Description
This book provides an accessible introduction to the fundamentals of civil and military aircraft design. 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. Following chapters explore structures, airframe systems, avionics and weapons systems. Later chapters examine the costs involved in the acquisition and operation of new aircraft, aircraft reliability and maintainability, and a variety of unsuccessful projects to see what conclusions can be drawn. Three appendices and a bibliography give a wealth of useful information, much not published elsewhere, including simple aerodynamic formulae, aircraft, engine and equipment data and a detailed description of a parametric study of a 500-seat transport aircraft.
Author: Jan Robert Wright Publisher: John Wiley & Sons ISBN: 047085846X Category : Technology & Engineering Languages : en Pages : 559
Book Description
Aeroelastic phenomena arising from the interaction of aerodynamic, elastic and inertia forces, and the loads resulting from flight / ground manoeuvres and gust / turbulence encounters, have a significant influence upon aircraft design. The prediction of aircraft aeroelastic stability, response and loads requires application of a range of interrelated engineering disciplines. This new textbook introduces the foundations of aeroelasticity and loads for the flexible aircraft, providing an understanding of the main concepts involved and relating them to aircraft behaviour and industrial practice. This book includes the use of simplified mathematical models to demonstrate key aeroelastic and loads phenomena including flutter, divergence, control effectiveness and the response and loads resulting from flight / ground manoeuvres and gust / turbulence encounters. It provides an introduction to some up-to-date methodologies for aeroelastics and loads modelling. It lays emphasis on the strong link between aeroelasticity and loads. It also includes provision of MATLAB and SIMULINK programs for the simplified analyses. It offers an overview of typical industrial practice in meeting certification requirements.
Author: Kevin High Publisher: ISBN: 9781933189796 Category : Languages : en Pages : 446
Book Description
This book introduces aircraft to students in any aviation-related track of study, whether they are future mechanics/technicians, pilots, or aviation managers. High school programs will also find this book useful for teaching the basics about aircraft.Readers get an excellent overview of aircraft structures and systems. And a substantial portion of the book is devoted to reciprocating and turbine powerplants and the systems that support them. Similar books offered in the past are out of print, out of date, and some ignore turbine engines. Throughout, this book explains the newest technologies and the tried-and-true ones that are still used. It is easy to understand, heavily illustrated, and has many photographs-all to enhance learning.Topics include aircraft structures; flight controls and flaps; electrical systems; hydraulic systems; landing gear, wheels, tires, and brakes; fuel systems; cabin atmosphere; instrument systems; ice, rain, smoke, and fire protection systems; aircraft powerplants overview; reciprocating engines; reciprocating engine systems; turbine engines and systems; and aircraft maintenance and documentation
Author: T.H.G. Megson Publisher: Butterworth-Heinemann ISBN: 1856179338 Category : Technology & Engineering Languages : en Pages : 645
Book Description
Introduction to Aircraft Structural Analysis is an essential resource for learning aircraft structural analysis. Based on the author's best-selling book Aircraft Structures for Engineering Students, this brief text introduces the reader to the basics of structural analysis as applied to aircraft structures. Coverage of elasticity, energy methods and virtual work sets the stage for discussions of airworthiness/airframe loads and stress analysis of aircraft components. Numerous worked examples, illustrations, and sample problems show how to apply the concepts to realistic situations. The book covers the core concepts in about 200 fewer pages by removing some optional topics like structural vibrations and aero elasticity. It consists of 23 chapters covering a variety of topics from basic elasticity to torsion of solid sections; energy methods; matrix methods; bending of thin plates; structural components of aircraft; airworthiness; airframe loads; bending of open, closed, and thin walled beams; combined open and closed section beams; wing spars and box beams; and fuselage frames and wing ribs. This book will appeal to undergraduate and postgraduate students of aerospace and aeronautical engineering, as well as professional development and training courses. Based on the author's best-selling text Aircraft Structures for Engineering Students, this Intro version covers the core concepts in about 200 fewer pages by removing some optional topics like structural vibrations and aeroelasticity Systematic step by step procedures in the worked examples Self-contained, with complete derivations for key equations
Author: Francis J. Hale Publisher: John Wiley & Sons ISBN: Category : Technology & Engineering Languages : en Pages : 344
Book Description
A self-contained in-depth treatment of aircraft performance, designed for a first course in aeronautical or aerospace engineering for undergraduate engineers. Provides an understanding of why conventional aircraft look and fly the way they do. This well written text covers turbofan and turboprop propulsion, subjects often avoided in other texts. New to the text is the treatment of wind effects on aircraft. Includes illustrative examples and references to practical piloting procedures and the significance of parameters.
Author: Thomas R. Yechout
Author: Thomas R. Yechout
Author: Mario Asselin
Author: John P. Fielding
Author: Louis V. Schmidt
Author: Jan Robert Wright
Author: Kevin High
Author: 
Author: Steven A. Brandt
Author: T.H.G. Megson
Author: Francis J. Hale