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Modern Aerodynamic Methods for Direct and Inverse Applications, Wilson C. Chin


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Автор: Wilson C. Chin   (Уилсон К. Чин)
Название:  Modern Aerodynamic Methods for Direct and Inverse Applications
Перевод названия: Уилсон К. Чин: Современные аэродинамические методы для прямых и обратных приложений
ISBN: 9781119580560
Издательство: Wiley
Классификация:

ISBN-10: 1119580560
Обложка/Формат: Hardback
Страницы: 444
Вес: 0.77 кг.
Дата издания: 15.03.2019
Серия: Physics
Язык: English
Размер: 239 x 158 x 24
Читательская аудитория: Professional & vocational
Ключевые слова: Physics,Mechanical engineering & materials
Основная тема: Physics,Mechanical engineering & materials
Ссылка на Издательство: Link
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Поставляется из: Англии
Описание: Just when classic subject areas seem understood, the author, a Caltech, M.I.T. and Boeing trained aerodynamicist, raises profound questions over traditional formulations. Can shear flows be rigorously modeled using simpler potential-like methods versus Euler equation approaches? Why not solve aerodynamic inverse problems using rapid, direct or forward methods similar to those used to calculate pressures over specified airfoils? Can transonic supercritical flows be solved rigorously without type-differencing methods? How do oscillations affect transonic mean flows, which in turn influence oscillatory effects? Or how do hydrodynamic disturbances stabilize or destabilize mean shear flows? Is there an exact approach to calculating wave drag for modern supersonic aircraft? This new book, by a prolific fluid-dynamicist and mathematician who has published more than twenty research monographs, represents not just another contribution to aerodynamics, but a book that raises serious questions about traditionally accepted approaches and formulations - and provides new methods that solve longstanding problems of importance to the industry.

While both conventional and newer ideas are discussed, the presentations are readable and geared to advanced undergraduates with exposure to elementary differential equations and introductory aerodynamics principles. Readers are introduced to fundamental algorithms (with Fortran source code) for basic applications, such as subsonic lifting airfoils, transonic supercritical flows utilizing mixed differencing, models for inviscid shear flow aerodynamics, and so on - models they can extend to include newer effects developed in the second half of the book. Many of the newer methods have appeared over the years in various journals and are now presented with deeper perspective and integration.

This book helps readers approach the literature more critically. Rather than simply understanding an approach, for instance, the powerful type differencing behind transonic analysis, or the rationale behind conservative formulations, or the use of Euler equation methods for shear flow analysis when they are unnecessary, the author guides and motivates the user to ask why and why not and what if. And often, more powerful methods can be developed using no more than simple mathematical manipulations.

For example, Cauchy-Riemann conditions, which are powerful tools in subsonic airfoil theory, can be readily extended to handle compressible flows with shocks, rotational flows, and even three-dimensional wing flowfields, in a variety of applications, to produce powerful formulations that address very difficult problems. This breakthrough volume is certainly a must have on every engineers bookshelf.



Foundations of Aerodynamics - Bases of Aerodynamic  Design (WSE)

Автор: Kuethe
Название: Foundations of Aerodynamics - Bases of Aerodynamic Design (WSE)
ISBN: 0471129194 ISBN-13(EAN): 9780471129196
Издательство: Wiley
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Цена: 253390.00 T
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Описание: Like previous editions, this text has retained it`s excellent coverage of basic concepts and broad coverage of the major aspects of aerodynamics. Numerical techniques are described for computing invicid incompressible flow about airfoils and finite wings.

Optimum Aerodynamic Design & Parallel Navier-Stokes Computations ECARP — European Computational Aerodynamics Research Project

Автор: Jacques Periaux; Stephane Lanteri; Panagiotis Chav
Название: Optimum Aerodynamic Design & Parallel Navier-Stokes Computations ECARP — European Computational Aerodynamics Research Project
ISBN: 3322901955 ISBN-13(EAN): 9783322901958
Издательство: Springer
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Цена: 113190.00 T
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Описание: This volume entitled "European Computational Aerodynamics Research Project (ECARP)" contains the contributions of partners presented in two work- shops focused on the following areas: Task 3 on Optimum Design and Task 4.2 on Navier Stokes Flow algorithms on Massively Parallel Processors. ECARP has been supported by the European Union (EU) through the Indus- trial and Materials Technology Programme, Area 3 Aeronautics, with the Third Research Framework Programme (1990-1994). Part A of this volume is focused on computational constrained optimization as a follow up of the EU research project" Optimum Design in Aerodynamics," (AERO-S9-0026) dealing with more viscous flow based real applications. It pro- vides the reader with a set of optimization tools and referenced data useful in modern aerodynamic design. Task 3 of the project entitled "Optimum Design" brought together 13 Euro- pean partners from the academic and industrial aeronautic oriented community showing state of the art expertise in traditional automated optimization software on current computer technology to improve the capability to optimize aircraft shapes.

Simulation-Driven Aerodynamic Design Using Variable-Fidelity Models

Автор: Leifsson Leifur Et Al
Название: Simulation-Driven Aerodynamic Design Using Variable-Fidelity Models
ISBN: 1783266287 ISBN-13(EAN): 9781783266289
Издательство: World Scientific Publishing
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Цена: 152070.00 T
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Описание: Computer simulations is a fundamental tool of the design process in many engineering disciplines including aerospace engineering.

Higher Approximations in Aerodynamic Theory

Автор: Lighthill M. J., Lighthill Sir M. J.
Название: Higher Approximations in Aerodynamic Theory
ISBN: 0691626014 ISBN-13(EAN): 9780691626017
Издательство: Wiley
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Цена: 33790.00 T
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Описание: Part of the Princeton Aeronautical Paperback series designed to bring to students and research engineers outstanding portions of the twelve-volume High Speed Aerodynamics and Jet Propulsion series. These books have been prepared by direct reproduction of the text from the original series and no attempt has been made to provide introductory material

Portable Parallelization of Industrial Aerodynamic Applications (POPINDA)

Автор: Anton Sch?ller
Название: Portable Parallelization of Industrial Aerodynamic Applications (POPINDA)
ISBN: 3322865789 ISBN-13(EAN): 9783322865786
Издательство: Springer
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Цена: 93160.00 T
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Описание: This book contains the main results of the German project POPINDA. It surveys the state of the art of industrial aerodynamic design simulations on parallel systems. POPINDA is an acronym for Portable Parallelization of Industrial Aerodynamic Applications. This project started in late 1993. The research and development work invested in POPINDA corresponds to about 12 scientists working full-time for the three and a half years of the project. POPINDA was funded by the German Federal Ministry for Education, Science, Research and Technology (BMBF). The central goals of POPINDA were to unify and parallelize the block-structured aerodynamic flow codes of the German aircraft industry and to develop new algorithmic approaches to improve the efficiency and robustness of these programs. The philosophy behind these goals is that challenging and important numerical appli- cations such as the prediction of the 3D viscous flow around full aircraft in aerodynamic design can only be carried out successfully if the benefits of modern fast numerical solvers and parallel high performance computers are combined. This combination is a "conditio sine qua non" if more complex applications such as aerodynamic design optimization or fluid structure interaction problems have to be solved. When being solved in a standard industrial aerodynamic design process, such more complex applications even require a substantial further reduction of computing times. Parallel and vector computers on the one side and innovative numerical algorithms such as multigrid on the other have enabled impressive improvements in scientific computing in the last 15 years.

Recent Development of Aerodynamic Design Methodologies

Автор: Kozo Fujii; George Dulikravich
Название: Recent Development of Aerodynamic Design Methodologies
ISBN: 3322899543 ISBN-13(EAN): 9783322899545
Издательство: Springer
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Цена: 95770.00 T
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Описание: Computational Fluid Dynamics (CFD) has made remarkable progress in the last two decades and is becoming an important, if not inevitable, analytical tool for both fundamental and practical fluid dynamics research. The analysis of flow fields is important in the sense that it improves the researcher's understanding of the flow features. CFD analysis also indirectly helps the design of new aircraft and/or spacecraft. However, design methodologies are the real need for the development of aircraft or spacecraft. They directly contribute to the design process and can significantly shorten the design cycle. Although quite a few publications have been written on this subject, most of the methods proposed were not used in practice in the past due to an immature research level and restrictions due to the inadequate computing capabilities. With the progress of high-speed computers, the time has come for such methods to be used practically. There is strong evidence of a growing interest in the development and use of aerodynamic inverse design and optimization techniques. This is true, not only for aerospace industries, but also for any industries requiring fluid dynamic design. This clearly shows the matured engineering need for optimum aerodynamic shape design methodologies. Therefore, it seems timely to publish a book in which eminent researchers in this area can elaborate on their research efforts and discuss it in conjunction with other efforts.

Aerodynamic Shape Optimization Using Control Theory

Автор: Reuther James
Название: Aerodynamic Shape Optimization Using Control Theory
ISBN: 1288915616 ISBN-13(EAN): 9781288915613
Издательство: Неизвестно
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Цена: 71050.00 T
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Wind Tunnel Aerodynamic Tests of Six Airfoils for Use on Small Wind Turbines

Название: Wind Tunnel Aerodynamic Tests of Six Airfoils for Use on Small Wind Turbines
ISBN: 1249145945 ISBN-13(EAN): 9781249145943
Издательство: Неизвестно
Цена: 20000.00 T
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Theoretical Aerodynamic Analyses of Six Airfoils for Use on Small Wind Turbines

Название: Theoretical Aerodynamic Analyses of Six Airfoils for Use on Small Wind Turbines
ISBN: 124913420X ISBN-13(EAN): 9781249134206
Издательство: Неизвестно
Цена: 22990.00 T
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Structural Studies of Liquids and Glasses Using Aerodynamic Levitation

Автор: Thomas Farmer
Название: Structural Studies of Liquids and Glasses Using Aerodynamic Levitation
ISBN: 331936054X ISBN-13(EAN): 9783319360546
Издательство: Springer
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Цена: 87060.00 T
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Описание: Introduction.- Theory of Supercooled Liquids and Glasses.- Experimental Techniques.- Rare Earth Doped Barium Titanate Glass.- Liquid-Liquid Transitions in Y2O3-Al2O3.- Liquid Invar.- Indium Selenide.- Conclusions.

The Practical Calculation of the Aerodynamic Characteristics of Slender Finned Vehicles

Автор: Barrowman James S.
Название: The Practical Calculation of the Aerodynamic Characteristics of Slender Finned Vehicles
ISBN: 1288910460 ISBN-13(EAN): 9781288910465
Издательство: Неизвестно
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Цена: 71050.00 T
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