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Aerodynamics For Engineering Students

Author: E. L. Houghton
Publisher: Butterworth-Heinemann
ISBN: 0081002327
Size: 78.90 MB
Format: PDF, Kindle
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Aerodynamics for Engineering Students, Seventh Edition, is one of the world’s leading course texts on aerodynamics. It provides concise explanations of basic concepts, combined with an excellent introduction to aerodynamic theory. This updated edition has been revised with improved pedagogy and reorganized content to facilitate student learning, and includes new or expanded coverage in several important areas, such as hypersonic flow, UAV’s, and computational fluid dynamics. Provides contemporary applications and examples that help students see the link between everyday physical examples of aerodynamics and the application of aerodynamic principles to aerodynamic design Contains MATLAB-based computational exercises throughout, giving students practice in using industry-standard computational tools Includes examples in SI and Imperial units, reflecting the fact that the aerospace industry uses both systems of units Improved pedagogy, including more examples and end-of-chapter problems, and additional and updated MATLAB codes

Aerodynamics For Engineering Students

Author: Edward Lewis Houghton
Publisher: Elsevier
ISBN: 0080966322
Size: 33.37 MB
Format: PDF, Kindle
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Already one of the leading course texts on aerodynamics in the UK, the sixth edition welcomes a new US-based author team to keep the text current. The sixth edition has been revised to include the latest developments in compressible flow, computational fluid dynamics, and contemporary applications. Computational methods have been expanded and updated to reflect the modern approaches to aerodynamic design and research in the aeronautical industry and elsewhere, and new examples of 'the aerodynamics around you' have been added to link theory to practical understanding. NEW: Expanded coverage of compressible flow NEW: MATLAB(r) exercises throughout, to give students practice is using industry-standard computational tools. m-files available for download from companion website. NEW: contemporary applications and examples help students see the link between everyday physical examples of aerodynamics and the application of aerodynamic principles to aerodynamic design. NEW: additional examples and end of chapter exercises provide more problem-solving practice for students NEW: improved teaching support with powerpoint slides, solutions manual, m-files, and other resources to accompany the text

Aerodynamics For Engineering Students

Author: E. L. Houghton
Publisher: Elsevier
ISBN: 0080966330
Size: 38.92 MB
Format: PDF, ePub, Mobi
View: 2795
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Already one of the leading course texts on aerodynamics in the UK, the sixth edition welcomes a new US-based author team to keep the text current. The sixth edition has been revised to include the latest developments in compressible flow, computational fluid dynamics, and contemporary applications. Computational methods have been expanded and updated to reflect the modern approaches to aerodynamic design and research in the aeronautical industry and elsewhere, and new examples of ‘the aerodynamics around you’ have been added to link theory to practical understanding. Expanded coverage of compressible flow MATLAB(r) exercises throughout, to give students practice is using industry-standard computational tools. Contemporary applications and examples help students see the link between everyday physical examples of aerodynamics and the application of aerodynamic principles to aerodynamic design Additional examples and end of chapter exercises provide more problem-solving practice for students

Aerodynamics For Engineers

Author: John J. Bertin
Publisher: Pearson Education
ISBN: 9780273793274
Size: 20.57 MB
Format: PDF, ePub
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Revised to reflect the technological advances and modern application in aerodynamics, this edition merges fundamental fluid mechanics, experimental techniques, and computational fluid dynamics techniques to build a solid foundation for students in aerodynamic applications from low-speed flight through hypersonic flight.

Aircraft Structures For Engineering Students

Author: T.H.G. Megson
Publisher: Butterworth-Heinemann
ISBN: 0081009984
Size: 10.55 MB
Format: PDF
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Aircraft Structures for Engineering Students, Sixth Edition, is the leading self-contained aircraft structures course text. It covers all fundamental subjects, including elasticity, structural analysis, airworthiness and aeroelasticity. Now in its sixth edition, the author has expanded the book’s coverage of analysis and design of composite materials for use in aircraft, and has added new, real-world and design-based examples, along with new end-of-chapter problems of varying complexity. Expanded coverage of composite materials and structures New practical and design-based examples and problems throughout the text aid understanding and relate concepts to real world applications Updated and additional Matlab examples and exercises support use of computational tools in analysis and design Available online teaching and learning tools include downloadable Matlab code, solutions manual, and image bank of figures from the book

Theoretical Aerodynamics

Author: Ethirajan Rathakrishnan
Publisher: John Wiley & Sons
ISBN: 1118479378
Size: 70.68 MB
Format: PDF, Kindle
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Theoretical Aerodynamics is a user-friendly text for a full course on theoretical aerodynamics. The author systematically introduces aerofoil theory, its design features and performance aspects, beginning with the basics required, and then gradually proceeding to higher level. The mathematics involved is presented so that it can be followed comfortably, even by those who are not strong in mathematics. The examples are designed to fix the theory studied in an effective manner. Throughout the book, the physics behind the processes are clearly explained. Each chapter begins with an introduction and ends with a summary and exercises. This book is intended for graduate and advanced undergraduate students of Aerospace Engineering, as well as researchers and Designers working in the area of aerofoil and blade design. Provides a complete overview of the technical terms, vortex theory, lifting line theory, and numerical methods Presented in an easy-to-read style making full use of figures and illustrations to enhance understanding, and moves well simpler to more advanced topics Includes a complete section on fluid mechanics and thermodynamics, essential background topics to the theory of aerodynamics Blends the mathematical and physical concepts of design and performance aspects of lifting surfaces, and introduces the reader to the thin aerofoil theory, panel method, and finite aerofoil theory Includes a Solutions Manual for end-of-chapter exercises, and Lecture slides on the book's Companion Website

Aircraft Design Projects

Author: Lloyd R. Jenkinson
Publisher: Elsevier
ISBN: 0080498957
Size: 74.18 MB
Format: PDF, ePub, Mobi
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Written with students of aerospace or aeronautical engineering firmly in mind, this is a practical and wide-ranging book that draws together the various theoretical elements of aircraft design - structures, aerodynamics, propulsion, control and others - and guides the reader in applying them in practice. Based on a range of detailed real-life aircraft design projects, including military training, commercial and concept aircraft, the experienced UK and US based authors present engineering students with an essential toolkit and reference to support their own project work. All aircraft projects are unique and it is impossible to provide a template for the work involved in the design process. However, with the knowledge of the steps in the initial design process and of previous experience from similar projects, students will be freer to concentrate on the innovative and analytical aspects of their course project. The authors bring a unique combination of perspectives and experience to this text. It reflects both British and American academic practices in teaching aircraft design. Lloyd Jenkinson has taught aircraft design at both Loughborough and Southampton universities in the UK and Jim Marchman has taught both aircraft and spacecraft design at Virginia Tech in the US. * Demonstrates how basic aircraft design processes can be successfully applied in reality * Case studies allow both student and instructor to examine particular design challenges * Covers commercial and successful student design projects, and includes over 200 high quality illustrations

An Introduction To Theoretical And Computational Aerodynamics

Author: Jack Moran
Publisher: Courier Corporation
ISBN: 0486317536
Size: 16.83 MB
Format: PDF, ePub, Docs
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Concise text discusses properties of wings and airfoils in incompressible and primarily inviscid flow, viscid flows, panel methods, finite difference methods, and computation of transonic flows past thin airfoils. 1984 edition.

Applied Computational Aerodynamics

Author: Russell M. Cummings
Publisher: Cambridge University Press
ISBN: 1107053749
Size: 35.19 MB
Format: PDF
View: 3634
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This computational aerodynamics (CA) textbook is written at the undergraduate level, based on years of teaching focused on developing the engineering skills required to become an intelligent user of aerodynamic codes, unlike most available books which focus on learning how to write codes. This is done by taking advantage of CA codes that are now freely available and doing projects to learn the basic numerical and aerodynamic concepts require. The authors believe that new and vibrant ways to interact with CA are important in order to improve understanding of aerodynamics. This book includes a number of unique features to make studying Computational Aerodynamics more enjoyable. These include: • The computer programs used in the book's projects are all open source and accessible to students and practicing engineers alike on the book web site, www.cambridge.org/cummings • CA Concept Boxes appear throughout the book to make material more relevant and to provide interesting asides from the material at hand • Flow Visualization Boxes are used throughout the book to give readers the opportunity to "see" fluid dynamic flows first hand • Profiles of both experienced and beginning practitioners of CA are included throughout to give a more personal dimension to the practice of numerical simulations of aerodynamics • Best Practices summaries are included at the end of most chapters to provide real world guidelines for how CA is typically used • The website includes access to images, movies, programs, CA codes, additional material, and links to a variety of resources vital to the discussions contained within the book (www.cambridge.org/cummings)

Theory Of Lift

Author: G. D. McBain
Publisher: John Wiley & Sons
ISBN: 1118346289
Size: 42.20 MB
Format: PDF, Docs
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Starting from a basic knowledge of mathematics and mechanics gained in standard foundation classes, Theory of Lift: Introductory Computational Aerodynamics in MATLAB/Octave takes the reader conceptually through from the fundamental mechanics of lift to the stage of actually being able to make practical calculations and predictions of the coefficient of lift for realistic wing profile and planform geometries. The classical framework and methods of aerodynamics are covered in detail and the reader is shown how they may be used to develop simple yet powerful MATLAB or Octave programs that accurately predict and visualise the dynamics of real wing shapes, using lumped vortex, panel, and vortex lattice methods. This book contains all the mathematical development and formulae required in standard incompressible aerodynamics as well as dozens of small but complete working programs which can be put to use immediately using either the popular MATLAB or free Octave computional modelling packages. Key features: Synthesizes the classical foundations of aerodynamics with hands-on computation, emphasizing interactivity and visualization. Includes complete source code for all programs, all listings having been tested for compatibility with both MATLAB and Octave. Companion website (www.wiley.com/go/mcbain) hosting codes and solutions. Theory of Lift: Introductory Computational Aerodynamics in MATLAB/Octave is an introductory text for graduate and senior undergraduate students on aeronautical and aerospace engineering courses and also forms a valuable reference for engineers and designers.