Anatomy of the Aeroplane
The Anatomy of the Aeroplane is the first of a trilogy of textbooks, including The Design of the Aeroplane and Flying Qualities and Flight Testing of the Aeroplane, which have been described internationally as classics and required reading for professionals and students of aeronautics around the world. Together, they link theory and practical experience in the areas of aeronautical form and function, design, flying qualities and flight testing. The Anatomy concentrates on a broad landscape of physical principles and technological advances, among aeroplanes designed to meet specific operational requirements, from military strike to disaster relief. The new edition has been extensively updated since its first publication in 1966. It discusses critically the advantages and disadvantages of different subsonic and supersonic aerodynamic, propulsive and structural configurations of light to heavy aircraft; stealth technology; design for operation in surface (ground) effect; and fly-by-wire, fly-by-light and high-order control systems to achieve extreme agility. It is extensively illustrated with additional plates and drawings.
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Anatomy of the Aeroplane
The Anatomy of the Aeroplane is the first of a trilogy of textbooks, including The Design of the Aeroplane and Flying Qualities and Flight Testing of the Aeroplane, which have been described internationally as classics and required reading for professionals and students of aeronautics around the world. Together, they link theory and practical experience in the areas of aeronautical form and function, design, flying qualities and flight testing. The Anatomy concentrates on a broad landscape of physical principles and technological advances, among aeroplanes designed to meet specific operational requirements, from military strike to disaster relief. The new edition has been extensively updated since its first publication in 1966. It discusses critically the advantages and disadvantages of different subsonic and supersonic aerodynamic, propulsive and structural configurations of light to heavy aircraft; stealth technology; design for operation in surface (ground) effect; and fly-by-wire, fly-by-light and high-order control systems to achieve extreme agility. It is extensively illustrated with additional plates and drawings.
114.95 In Stock
Anatomy of the Aeroplane

Anatomy of the Aeroplane

by Darrol Stinton
Anatomy of the Aeroplane

Anatomy of the Aeroplane

by Darrol Stinton

Paperback(2ND)

$114.95 
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Overview

The Anatomy of the Aeroplane is the first of a trilogy of textbooks, including The Design of the Aeroplane and Flying Qualities and Flight Testing of the Aeroplane, which have been described internationally as classics and required reading for professionals and students of aeronautics around the world. Together, they link theory and practical experience in the areas of aeronautical form and function, design, flying qualities and flight testing. The Anatomy concentrates on a broad landscape of physical principles and technological advances, among aeroplanes designed to meet specific operational requirements, from military strike to disaster relief. The new edition has been extensively updated since its first publication in 1966. It discusses critically the advantages and disadvantages of different subsonic and supersonic aerodynamic, propulsive and structural configurations of light to heavy aircraft; stealth technology; design for operation in surface (ground) effect; and fly-by-wire, fly-by-light and high-order control systems to achieve extreme agility. It is extensively illustrated with additional plates and drawings.

Product Details

ISBN-13: 9780632040292
Publisher: Wiley
Publication date: 08/24/1998
Edition description: 2ND
Pages: 480
Product dimensions: 3.94(w) x 9.84(h) x 0.59(d)

About the Author

Darrol Stinton is the author of Anatomy of the Aeroplane, 2nd Edition, published by Wiley.

Table of Contents

Part 1 - Environment. The atmosphere; The operational environment; Part 2 - Requirements. Requirements and the specification; Interpretation of requirements; Part 3 - Aerodynamic Shape. The 'Classical' generation of aerodynamic forces; The control of lift and drag; Engine-airframe matching; Balancing the aerodynamic sum; Part 4 - Ground and Water Operations. Landplanes; Seaplanes; The structure; The final aeroplane; Appendices; References and further reading; Index.
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