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Author : Michael S. Selig
Publisher : Soartech
Page : 320 pages
File Size : 55,7 Mb
Release : 1995
Category : Technology & Engineering
ISBN : STANFORD:36105115142486
Author : Anonim
Publisher : Unknown
Page : 440 pages
File Size : 42,6 Mb
Release : 1997
Category : Aerodynamics
ISBN : 0964674734
Author : Christopher A. Lyon,Michael S. Selig
Publisher : Unknown
Page : 962 pages
File Size : 52,5 Mb
Release : 1997
Category : Electronic
ISBN : 0964674734
Author : Michael S. Selig
Publisher : Unknown
Page : 95 pages
File Size : 48,8 Mb
Release : 1995
Category : Aerodynamics
ISBN : OCLC:814380608
Author : Joseph Katz,Allen Plotkin
Publisher : Cambridge University Press
Page : 636 pages
File Size : 41,8 Mb
Release : 2001-02-05
Category : Mathematics
ISBN : 0521665523
A treatment of low-speed aerodynamics, covering both theory and computational techniques, first published in 2001.
Author : Tuncer Cebeci,Max Platzer,Hsun Chen,Kuo-cheng Chang,Jian P. Shao
Publisher : Springer
Page : 0 pages
File Size : 50,9 Mb
Release : 2014-11-16
Category : Technology & Engineering
ISBN : 3642444962
The standard textbooks on aerodynamics usually omit any discussion of un steady aerodynamics or, at most, consider it only in a single chapter, based on two justifications. The first is that unsteady aerodynamics should be regarded as a specialized subject required "only" in connection with understanding and an alyzing aeroelastic phenomena such as flutter and gust response, and therefore should be dealt with in related specialist books. The second reason appears to be reluctance to discuss aerodynamics with the inclusion of the time-dependent terms in the conservation equations and the boundary conditions for fear that added complications may discourage the reader. We take the opposite view in this book and argue that a full understanding of the physics of lift generation is possible only by considering the unsteady aerody namics of the starting vortex generation process. Furthermore, certain "steady" flows are inherently unsteady in the presence of flow separation, as for example the unsteady flow caused by the Karman vortex shedding downstream of a cylin der and "static" airfoil stall which is an inherently unsteady flow phenomenon. Therefore, it stands to reason that a unified treatment of aerodynamics that yields steady-state aerodynamics as a special case offers advantages. This rea soning is strengthened by the developments in computational fluid dynamics over the past forty years, which showed that accurate steady-state solutions can be obtained efficiently by solving the unsteady flow equations.
Author : Richard A. Eppler,Dan M. Somers
Publisher : Unknown
Page : 152 pages
File Size : 42,5 Mb
Release : 1980
Category : Aerofoils
ISBN : UIUC:30112106660670
Author : Michael S. Selig,John Francis Donovan,David Bruce Fraser
Publisher : Unknown
Page : 424 pages
File Size : 50,8 Mb
Release : 1989
Category : Aerodynamics
ISBN : STANFORD:36105021561332
Author : Ira H. Abbott,A. E. von Doenhoff
Publisher : Courier Corporation
Page : 704 pages
File Size : 55,9 Mb
Release : 2012-04-26
Category : Technology & Engineering
ISBN : 9780486134994
Concise compilation of subsonic aerodynamic characteristics of NACA wing sections, plus description of theory. 350 pages of tables.
Author : Bernhard Stoevesandt,Gerard Schepers,Peter Fuglsang,Yuping Sun
Publisher : Springer Nature
Page : 1495 pages
File Size : 42,9 Mb
Release : 2022-08-04
Category : Technology & Engineering
ISBN : 9783030313074
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.
Author : R.W. Barnwell,M.Y. Hussaini
Publisher : Springer Science & Business Media
Page : 415 pages
File Size : 53,6 Mb
Release : 2012-12-06
Category : Science
ISBN : 9781461228721
Research on laminar flow and its transition to turbulent flow has been an important part of fluid dynamics research during the last sixty years. Since transition impacts, in some way, every aspect of aircraft performance, this emphasis is not only understandable but should continue well into the future. The delay of transition through the use of a favorable pressure gradient by proper body shaping (natural laminar flow) or the use of a small amount of suction (laminar flow control) was recognized even in the early 1930s and rapidly became the foundation of much of the laminar flow research in the U.S. and abroad. As one would expect, there have been many approaches, both theoretical and experimental, employed to achieve the substantial progress made to date. Boundary layer stability theories have been formu lated and calibrated by a good deal of wind tunnel and flight experiments. New laminar now airfoils and wings have been designed and many have been employed in aircraft designs. While the early research was, of necessity, concerned with the design of subsonic aircraft interest has steadily moved to higher speeds including those appropriate to planetary entry. Clearly, there have been substantial advances in our understanding of transition physics and in the development and application of transition prediction methodolo gies to the design of aircraft.
Author : Edward Lewis Houghton
Publisher : Unknown
Page : 458 pages
File Size : 41,9 Mb
Release : 1978
Category : Electronic
ISBN : OCLC:916190858
Author : Mark Drela
Publisher : MIT Press
Page : 304 pages
File Size : 40,5 Mb
Release : 2014-02-07
Category : Science
ISBN : 9780262526449
An overview of the physics, concepts, theories, and models underlying the discipline of aerodynamics. This book offers a general overview of the physics, concepts, theories, and models underlying the discipline of aerodynamics. A particular focus is the technique of velocity field representation and modeling via source and vorticity fields and via their sheet, filament, or point-singularity idealizations. These models provide an intuitive feel for aerodynamic flow-field behavior and are the basis of aerodynamic force analysis, drag decomposition, flow interference estimation, and other important applications. The models are applied to both low speed and high speed flows. Viscous flows are also covered, with a focus on understanding boundary layer behavior and its influence on aerodynamic flows. The book covers some topics in depth while offering introductions and summaries of others. Computational methods are indispensable for the practicing aerodynamicist, and the book covers several computational methods in detail, with a focus on vortex lattice and panel methods. The goal is to improve understanding of the physical models that underlie such methods. The book also covers the aerodynamic models that describe the forces and moments on maneuvering aircraft, and provides a good introduction to the concepts and methods used in flight dynamics. It also offers an introduction to unsteady flows and to the subject of wind tunnel measurements. The book is based on the MIT graduate-level course “Flight Vehicle Aerodynamics” and has been developed for use not only in conventional classrooms but also in a massive open online course (or MOOC) offered on the pioneering MOOC platform edX. It will also serve as a valuable reference for professionals in the field. The text assumes that the reader is well versed in basic physics and vector calculus, has had some exposure to basic fluid dynamics and aerodynamics, and is somewhat familiar with aerodynamics and aeronautics terminology.
Author : Jewel B. Barlow,William H. Rae,Alan Pope
Publisher : John Wiley & Sons
Page : 738 pages
File Size : 43,5 Mb
Release : 1999-02-22
Category : Technology & Engineering
ISBN : 9780471557746
A brand-new edition of the classic guide on low-speed wind tunnel testing While great advances in theoretical and computational methods have been made in recent years, low-speed wind tunnel testing remains essential for obtaining the full range of data needed to guide detailed design decisions for many practical engineering problems. This long-awaited Third Edition of William H. Rae, Jr.'s landmark reference brings together essential information on all aspects of low-speed wind tunnel design, analysis, testing, and instrumentation in one easy-to-use resource. Written by authors who are among the most respected wind tunnel engineers in the world, this edition has been updated to address current topics and applications, and includes coverage of digital electronics, new instrumentation, video and photographic methods, pressure-sensitive paint, and liquid crystal-based measurement methods. The book is organized for quick access to topics of interest, and examines basic test techniques and objectives of modeling and testing aircraft designs in low-speed wind tunnels, as well as applications to fluid motion analysis, automobiles, marine vessels, buildings, bridges, and other structures subject to wind loading. Supplemented with real-world examples throughout, Low-Speed Wind Tunnel Testing, Third Edition is an indispensable resource for aerospace engineering students and professionals, engineers and researchers in the automotive industries, wind tunnel designers, architects, and others who need to get the most from low-speed wind tunnel technology and experiments in their work.
Author : Cliff Matthews
Publisher : Elsevier
Page : 288 pages
File Size : 43,9 Mb
Release : 2001-10-17
Category : Technology & Engineering
ISBN : 9780080488288
Aeronautical Engineer's Data Bookis an essential handy guide containing useful up to date information regularly needed by the student or practising engineer. Covering all aspects of aircraft, both fixed wing and rotary craft, this pocket book provides quick access to useful aeronautical engineering data and sources of information for further in-depth information. Quick reference to essential data Most up to date information available