Airfoil Design and Data

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Author :
Publisher : Springer Science & Business Media
ISBN 13 : 3662026465
Total Pages : 569 pages
Book Rating : 4.6/5 (62 download)

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Book Synopsis Airfoil Design and Data by : Richard Eppler

Download or read book Airfoil Design and Data written by Richard Eppler and published by Springer Science & Business Media. This book was released on 2012-12-06 with total page 569 pages. Available in PDF, EPUB and Kindle. Book excerpt: This detailed book describes a procedure for the design and analysis of subsonic airfoils. Contains 116 new airfoils for a wide range of Reynolds numbers and application requirements, including the input data for the computer code.

Summary of Low Speed Airfoil Data

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Author :
Publisher : Soartech
ISBN 13 :
Total Pages : 320 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Summary of Low Speed Airfoil Data by : Michael S. Selig

Download or read book Summary of Low Speed Airfoil Data written by Michael S. Selig and published by Soartech. This book was released on 1995 with total page 320 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Computer Program for the Design and Analysis of Low-speed Airfoils

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Author :
Publisher :
ISBN 13 :
Total Pages : 152 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis A Computer Program for the Design and Analysis of Low-speed Airfoils by : Richard A. Eppler

Download or read book A Computer Program for the Design and Analysis of Low-speed Airfoils written by Richard A. Eppler and published by . This book was released on 1980 with total page 152 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Low Reynolds Number Aerodynamics

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Publisher : Springer Science & Business Media
ISBN 13 : 3642840108
Total Pages : 456 pages
Book Rating : 4.6/5 (428 download)

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Book Synopsis Low Reynolds Number Aerodynamics by : Thomas J. Mueller

Download or read book Low Reynolds Number Aerodynamics written by Thomas J. Mueller and published by Springer Science & Business Media. This book was released on 2013-03-08 with total page 456 pages. Available in PDF, EPUB and Kindle. Book excerpt: Current interest in a variety of low Reynolds number applications has focused attention on the design and evaluation of efficient airfoil sections at chord Reynolds numbers from about 100,000 to about 1,000,000. These applications include remotely piloted vehicles (RPVs) at high altitudes, sailplanes, ultra-light man-carrying/man powered aircraft, mini-RPVs at low altitudes and wind turbines/propellers. The purpose of this conference was to bring together those researchers who have been active in areas closely related to this subject. All of the papers presented are research type papers. Main topics are: Airfoil Design and Analysis, Computational Studies, Stability and Transition, Laminar Separation Bubble, Steady and Unsteady Wind Tunnel Experiments and Flight Experiments.

Theory of Wing Sections

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Publisher : Courier Corporation
ISBN 13 : 0486134997
Total Pages : 708 pages
Book Rating : 4.4/5 (861 download)

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Book Synopsis Theory of Wing Sections by : Ira H. Abbott

Download or read book Theory of Wing Sections written by Ira H. Abbott and published by Courier Corporation. This book was released on 2012-04-26 with total page 708 pages. Available in PDF, EPUB and Kindle. Book excerpt: Concise compilation of subsonic aerodynamic characteristics of NACA wing sections, plus description of theory. 350 pages of tables.

Basic Wing and Airfoil Theory

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Author :
Publisher :
ISBN 13 : 9781258206772
Total Pages : 312 pages
Book Rating : 4.2/5 (67 download)

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Book Synopsis Basic Wing and Airfoil Theory by : Alan Pope

Download or read book Basic Wing and Airfoil Theory written by Alan Pope and published by . This book was released on 2011-10-01 with total page 312 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Airfoils at Low Speeds

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Publisher :
ISBN 13 :
Total Pages : 424 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Airfoils at Low Speeds by : Michael S. Selig

Download or read book Airfoils at Low Speeds written by Michael S. Selig and published by . This book was released on 1989 with total page 424 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aircraft Performance

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Publisher : Cambridge University Press
ISBN 13 : 9780521568364
Total Pages : 334 pages
Book Rating : 4.5/5 (683 download)

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Book Synopsis Aircraft Performance by : W. Austyn Mair

Download or read book Aircraft Performance written by W. Austyn Mair and published by Cambridge University Press. This book was released on 1996-03-14 with total page 334 pages. Available in PDF, EPUB and Kindle. Book excerpt: Describes the principles and equations required for evaluating the performance of an aircraft.

Aircraft Design

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Publisher : John Wiley & Sons
ISBN 13 : 1118352807
Total Pages : 811 pages
Book Rating : 4.1/5 (183 download)

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Book Synopsis Aircraft Design by : Mohammad H. Sadraey

Download or read book Aircraft Design written by Mohammad H. Sadraey and published by John Wiley & Sons. This book was released on 2012-11-20 with total page 811 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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

Aircraft Aerodynamic Design with Computational Software

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Publisher : Cambridge University Press
ISBN 13 : 1107019486
Total Pages : 467 pages
Book Rating : 4.1/5 (7 download)

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Book Synopsis Aircraft Aerodynamic Design with Computational Software by : Arthur Rizzi

Download or read book Aircraft Aerodynamic Design with Computational Software written by Arthur Rizzi and published by Cambridge University Press. This book was released on 2021-05-20 with total page 467 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerodynamic design of aircraft presented with realistic applications, using CFD software. Tutorials, exercises, and mini-projects provided involve design of real aircraft. Using online resources and supplements, this text prepares last-year undergraduates and first-year graduate students for industrial aerospace design and analysis tasks.

Basic Aerodynamics

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Publisher : Cambridge University Press
ISBN 13 : 1139498614
Total Pages : 433 pages
Book Rating : 4.1/5 (394 download)

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Book Synopsis Basic Aerodynamics by : Gary A. Flandro

Download or read book Basic Aerodynamics written by Gary A. Flandro and published by Cambridge University Press. This book was released on 2011-11-14 with total page 433 pages. Available in PDF, EPUB and Kindle. Book excerpt: In the rapidly advancing field of flight aerodynamics, it is especially important for students to master the fundamentals. This text, written by renowned experts, clearly presents the basic concepts of underlying aerodynamic prediction methodology. These concepts are closely linked to physical principles so that they are more readily retained and their limits of applicability are fully appreciated. Ultimately, this will provide students with the necessary tools to confidently approach and solve practical flight vehicle design problems of current and future interest. This book is designed for use in courses on aerodynamics at an advanced undergraduate or graduate level. A comprehensive set of exercise problems is included at the end of each chapter.

Handbook of Wind Energy Aerodynamics

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Author :
Publisher : Springer Nature
ISBN 13 : 3030313077
Total Pages : 1495 pages
Book Rating : 4.0/5 (33 download)

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Book Synopsis Handbook of Wind Energy Aerodynamics by : Bernhard Stoevesandt

Download or read book Handbook of Wind Energy Aerodynamics written by Bernhard Stoevesandt and published by Springer Nature. This book was released on 2022-08-04 with total page 1495 pages. Available in PDF, EPUB and Kindle. Book excerpt: This handbook provides both a comprehensive overview and deep insights on the state-of-the-art methods used in wind turbine aerodynamics, as well as their advantages and limits. The focus of this work is specifically on wind turbines, where the aerodynamics are different from that of other fields due to the turbulent wind fields they face and the resultant differences in structural requirements. It gives a complete picture of research in the field, taking into account the different approaches which are applied. This book would be useful to professionals, academics, researchers and students working in the field.

The Enigma of the Aerofoil

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Author :
Publisher : University of Chicago Press
ISBN 13 : 0226060934
Total Pages : 562 pages
Book Rating : 4.2/5 (26 download)

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Book Synopsis The Enigma of the Aerofoil by : David Bloor

Download or read book The Enigma of the Aerofoil written by David Bloor and published by University of Chicago Press. This book was released on 2011-10-03 with total page 562 pages. Available in PDF, EPUB and Kindle. Book excerpt: Why do aircraft fly? How do their wings support them? In the early years of aviation, there was an intense dispute between British and German experts over the question of why and how an aircraft wing provides lift. The British, under the leadership of the great Cambridge mathematical physicist Lord Rayleigh, produced highly elaborate investigations of the nature of discontinuous flow, while the Germans, following Ludwig Prandtl in Göttingen, relied on the tradition called “technical mechanics” to explain the flow of air around a wing. Much of the basis of modern aerodynamics emerged from this remarkable episode, yet it has never been subject to a detailed historical and sociological analysis. In The Enigma of the Aerofoil, David Bloor probes a neglected aspect of this important period in the history of aviation. Bloor draws upon papers by the participants—their restricted technical reports, meeting minutes, and personal correspondence, much of which has never before been published—and reveals the impact that the divergent mathematical traditions of Cambridge and Göttingen had on this great debate. Bloor also addresses why the British, even after discovering the failings of their own theory, remained resistant to the German circulation theory for more than a decade. The result is essential reading for anyone studying the history, philosophy, or sociology of science or technology—and for all those intrigued by flight.

Airfoil Selection

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Publisher :
ISBN 13 : 9787770045257
Total Pages : 0 pages
Book Rating : 4.0/5 (452 download)

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Book Synopsis Airfoil Selection by : Barnaby Wainfan

Download or read book Airfoil Selection written by Barnaby Wainfan and published by . This book was released on 2005 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Applied Computational Aerodynamics

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Publisher : AIAA
ISBN 13 : 9781600863790
Total Pages : 970 pages
Book Rating : 4.8/5 (637 download)

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Book Synopsis Applied Computational Aerodynamics by : P. A. Henne

Download or read book Applied Computational Aerodynamics written by P. A. Henne and published by AIAA. This book was released on 1990 with total page 970 pages. Available in PDF, EPUB and Kindle. Book excerpt:

US Army Helicopter Design Datcom: Airfoils

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Publisher :
ISBN 13 :
Total Pages : 310 pages
Book Rating : 4.0/5 ( download)

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Book Synopsis US Army Helicopter Design Datcom: Airfoils by : L. U. Dadone

Download or read book US Army Helicopter Design Datcom: Airfoils written by L. U. Dadone and published by . This book was released on 1976 with total page 310 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Fundamentals of Aircraft and Airship Design

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Publisher : AIAA (American Institute of Aeronautics & Astronautics)
ISBN 13 :
Total Pages : 940 pages
Book Rating : 4.3/5 (97 download)

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Book Synopsis Fundamentals of Aircraft and Airship Design by : Leland Malcolm Nicolai

Download or read book Fundamentals of Aircraft and Airship Design written by Leland Malcolm Nicolai and published by AIAA (American Institute of Aeronautics & Astronautics). This book was released on 2010 with total page 940 pages. Available in PDF, EPUB and Kindle. Book excerpt: The aircraft is only a transport mechanism for the payload, and all design decisions must consider payload first. Simply stated, the aircraft is a dust cover. "Fundamentals of Aircraft and Airship Design, Volume 1: Aircraft Design" emphasizes that the science and art of the aircraft design process is a compromise and that there is no right answer; however, there is always a best answer based on existing requirements and available technologies.