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Fluid Mechanics in Channel, Pipe and Aerodynamic Design Geometries 1, Christina G. Georgantopoulou, George A. Georgantop


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Автор: Christina G. Georgantopoulou, George A. Georgantop   (Кристина Г. Географтопуло)
Название:  Fluid Mechanics in Channel, Pipe and Aerodynamic Design Geometries 1
Перевод названия: Кристина Г. Географтопуло: Жидкостная механика в геометрии каналов, труб и аэродинамических конструк
ISBN: 9781786301390
Издательство: Wiley
Классификация:


ISBN-10: 1786301393
Обложка/Формат: Hardcover
Страницы: 412
Вес: 0.74 кг.
Дата издания: 28.03.2018
Серия: Mechanical engineering & materials
Язык: English
Издание: Volume 1
Размер: 243 x 166 x 27
Читательская аудитория: Professional & vocational
Ключевые слова: Mechanical engineering & materials
Основная тема: Mechanical engineering & materials
Ссылка на Издательство: Link
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Поставляется из: Англии
Описание:

Fluid mechanics is an important scientific field with various industrial applications for flows or energy consumption and efficiency issues. This book has as main aim to be a textbook of applied knowledge in real fluids as well as to the Hydraulic systems components and operation, with emphasis to the industrial or real life problems for piping and aerodynamic design geometries. Various problems will be presented and analyzed through this book.




MEGADESIGN and MegaOpt - German Initiatives for Aerodynamic Simulation and Optimization in Aircraft Design

Автор: Norbert Kroll; Dieter Schwamborn; Klaus Becker; He
Название: MEGADESIGN and MegaOpt - German Initiatives for Aerodynamic Simulation and Optimization in Aircraft Design
ISBN: 3642040926 ISBN-13(EAN): 9783642040924
Издательство: Springer
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Цена: 47377.00 р.
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Описание: Reduction of Simulation Time.- Recent Developments of TAU Adaptation Capability.- Adaptive Wall Function for the Prediction of Turbulent Flows.- Acceleration of CFD Processes for Transport Aircraft.- Efficient Combat Aircraft Simulations with the TAU RANS Code.- Improvement of Simulation Quality.- Universal Wall Functions for Aerodynamic Flows: Turbulence Model Consistent Design, Potential and Limitations.- Computational Modelling of Transonic Aerodynamic Flows Using Near-Wall, Reynolds Stress Transport Models.- Transition Prediction for Three-Dimensional Configurations.- Application of Transition Prediction.- Numerical Simulation Quality Assessment for Transport Aircraft.- Fluid Structure Coupling.- Computational Methods for Aero-Structural Analysis and Optimisation of Aircrafts Based on Reduced-Order Structural Models.- Development and Application of TAU-ANSYS Coupling Procedure.- Fluid-Structure Coupling: Simplified Structural Model on Complex Configurations.- Improvement of Shape Optimization Strategies.- Development of an Automated Artificial Neural Network for Numerical Optimization.- modeFRONTIER(c), a Framework for the Optimization of Military Aircraft Configurations.- One-Shot Methods for Aerodynamic Shape Optimization.- Automatic Differentiation of FLOWer and MUGRIDO.- Adjoint Methods for Coupled CFD-CSM Optimization.- Aerodynamic and Multidisciplinary Optimization of 3D-Configurations.- Aerodynamic Optimization for Cruise and High-Lift Configurations.- Aerodynamic Optimization of an UCAV Configuration.- Flexible Wing Optimisation Based on Shapes and Structures.- Multidisciplinary Optimization of an UAV Combining CFD and CSM.

MEGADESIGN and MegaOpt - German Initiatives for Aerodynamic Simulation and Optimization in Aircraft Design

Автор: Norbert Kroll; Dieter Schwamborn; Klaus Becker; He
Название: MEGADESIGN and MegaOpt - German Initiatives for Aerodynamic Simulation and Optimization in Aircraft Design
ISBN: 3642260624 ISBN-13(EAN): 9783642260629
Издательство: Springer
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Цена: 47377.00 р.
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Описание: Contains results of the German CFD initiative megadesign which combines CFD development activities from DLR, universities and aircraft industry. This title highlights improvements and enhancements of the flow solvers as well as developments with respect to aerodynamic and multidisciplinary shape optimization.

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: 14365.00 р.
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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 Drag Reduction Technologies

Автор: Peter Thiede
Название: Aerodynamic Drag Reduction Technologies
ISBN: 364207541X ISBN-13(EAN): 9783642075414
Издательство: Springer
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Цена: 39182.00 р.
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Описание: This volume contains the proceedings of the CEASlDragNet European Drag Reduction Conference held on 19-21 June 2000 in Potsdam, Germany. This conference, succeeding the First and Second European Forum on Laminar Flow Technology 1992 and 1996 respectively, was initiated by the European Drag Reduction Network (DragNet) and organised by DGLR (Deutsche Gesellschaft fUr Luft- und Raumfahrt - Lilienthal Oberth e. V. ) under the auspices ofCEAS (Confederation of European Aerospace Societies). The development of aerodynamic drag reduction technologies is driven by predictions of remarkable fuel savings, promising substantial improvements not only of aircraft efficiency but also of environmental compatibility. However, considerable efforts on an European scale are needed in order to develop, qualifY and demonstrate the means for their practical realisation. The primary aim of this conference was to provide a comprehensive survey of the current status of research, development and application in all disciplines of aerodynamic drag re- duction including laminar flow technology, adaptive wing concepts, turbulence and se- paration control, induced drag reduction and supersonic flow aspects. Besides aerodynamic topics the Call for Papers addressed also interdisciplinary aspects of design & system inte- gration, structures, materials, manufacturing, operations and maintenance. The Programme Committee (PC), responsible for the scientific preparation of the conference, consisted of CEAS representatives and DragNet board members (see following page).

Numerical and Phyical Aspects of Aerodynamic Flow III

Автор: T. Cebeci
Название: Numerical and Phyical Aspects of Aerodynamic Flow III
ISBN: 1461293626 ISBN-13(EAN): 9781461293620
Издательство: Springer
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Цена: 14673.00 р.
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Описание: In this volume, the emphasis is on three-dimensional flows with a section of five papers concerned with unsteady flows and a section of seven papers on three- dimensional flows: The papers deal mainly with calculation methods and encompass subsonic and transonic, attached and separated flows.

Aerodynamic Data of Space Vehicles

Автор: Claus Weiland
Название: Aerodynamic Data of Space Vehicles
ISBN: 366252046X ISBN-13(EAN): 9783662520468
Издательство: Springer
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Цена: 18284.00 р.
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Описание: This book details the aerodynamics of more than 25 vehicles. It provides readers with insight into the aerodynamics of various flight configurations.

Numerical and Physical Aspects of Aerodynamic Flows IV

Автор: Tuncer Cebeci
Название: Numerical and Physical Aspects of Aerodynamic Flows IV
ISBN: 3662026457 ISBN-13(EAN): 9783662026458
Издательство: Springer
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Описание: This volume contains a selection of the papers presented at the Fourth Symposium on Numerical and Physical Aspects of Aerodynamic Flows, which was held at the California State University, Long Beach, from 16-19 January 1989.

Aerodynamic Noise

Автор: Tarit Bose
Название: Aerodynamic Noise
ISBN: 1493901966 ISBN-13(EAN): 9781493901968
Издательство: Springer
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Цена: 11753.00 р.
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Описание: This book covers the theoretical basis and mathematical modeling of sound, especially undesirable sounds produced by aircraft, such as engine noise from propellers, fans, combustion chamber and jets, external surface noise and sonic booms. Offers problem sets.

Probability-Based Structural Fire Load

Автор: Razdolsky
Название: Probability-Based Structural Fire Load
ISBN: 110703874X ISBN-13(EAN): 9781107038745
Издательство: Cambridge Academ
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Цена: 19800.00 р.
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Описание: Probability-Based Structural Fire Load introduces the subject of probabilistic analysis to engineers and can also act as a reference to guide those applying this technology. In addition to providing an understanding of how fire affects structures, this book provides guidance for design professionals and is a resource for educators.

An Introduction to Noncommutative Spaces and Their Geometries

Автор: Giovanni Landi
Название: An Introduction to Noncommutative Spaces and Their Geometries
ISBN: 3662141094 ISBN-13(EAN): 9783662141090
Издательство: Springer
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Цена: 11753.00 р.
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Описание: These lecture notes are an introduction to several ideas and applications of noncommutative geometry. It starts with a not necessarily commutative but associative algebra which is thought of as the algebra of functions on some `virtual noncommutative space`.

Buoyancy-Thermocapillary Convection of Volatile Fluids in Confined and Sealed Geometries

Автор: Tongran Qin
Название: Buoyancy-Thermocapillary Convection of Volatile Fluids in Confined and Sealed Geometries
ISBN: 3319613308 ISBN-13(EAN): 9783319613307
Издательство: Springer
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Цена: 16769.00 р.
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Описание:

CHAPTER 1 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . 1

1.1 Motivation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

1.2 Previous Studies . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3

1.2.1 Buoyancy-Thermocapillary Convection . . . . . . . . . . . . . . 3

1.2.2 Modeling of Two-Phase Cooling Devices . . . . . . . . . . . . . 7

1.2.3 Effect of Noncondensable Gases . . . . . . . . . . . . . . . . . . 14

1.2.4 Direct Numerical Simulation of Two-Phase Flows . . . . . . . . . 18

1.3 Objectives of This Work . . . . . . . . . . . . . . . . . . . . . . . . . . . 20

CHAPTER 2 MATHEMATICAL MODEL . . . . . . . . . . . . . . . . . . . . 24

2.1 Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 24

2.2 Fundamental Equations for Simple Fluid Flow . . . . . . . . . . . . . . . 25

2.3 Fundamental Equations for Binary Fluid Flow . . . . . . . . . . . . . . . 26

2.4 Constitutive Relations . . . . . . . . . . . . . . . . . . . . . . . . . . . . 28

2.4.1 Equations of State . . . . . . . . . . . . . . . . . . . . . . . . . . 29

2.4.2 Molecular Diffusion . . . . . . . . . . . . . . . . . . . . . . . . . 30

2.4.3 Material Parameters . . . . . . . . . . . . . . . . . . . . . . . . . 31

2.5 Simplified Form of the Governing Equations . . . . . . . . . . . . . . . . 33

2.6 Boundary Conditions . . . . . . . . . . . . . . . . . . . . . . . . . . . . 35

2.6.1 Liquid-Gas Interface . . . . . . . . . . . . . . . . . . . . . . . . 35

2.6.2 Inner Surface of the Cavity . . . . . . . . . . . . . . . . . . . . . 42

2.6.3 Solution Procedure . . . . . . . . . . . . . . . . . . . . . . . . . 42

CHAPTER 3 CONVECTION AT ATMOSPHERIC CONDITIONS . . . . . . 44

3.1 Numerical Results . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 46

3.1.1 Steady Unicellular and Multicellular Flow . . . . . . . . . . . . . 48

3.1.2 Oscillatory Multicellular Flow . . . . . . . . . . . . . . . . . . . 52

3.2 Comparison with Experiments . . . . . . . . . . . . . . . . . . . . . . . 54

3.3 The Effect of the Interfacial Curvature . . . . . . . . . . . . . . . . . . . 59

3.4 Three-Dimensional Effects . . . . . . . . . . . . . . . . . . . . . . . . . 61

3.5 Theoretical Analysis . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 66

3.5.1 Fluid Flow and Temperature in the Liquid Layer . . . . . . . . . . 71

3.5.2 Fluid Flow, Temperature, and Composition in the Gas Layer . . . 73

3.6 End Wall Effects . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 77

3.7 Validity of the One-Sided Models . . . . . . . . . . . . . . . . . . . . . . 79

3.7.1 Interface Shape . . . . . . . . . . . . . . . . . . . . . . . . . . . 79

3.7.2 Phase Change . . . . . . . . . . . . . . . . . . . . . . . . . . . . 80

3.7.3 Newton's Law of Cooling . . . . . . . . . . . . . . . . . . . . . . 82

3.8 Discussion . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 84

CHAPTER 4 CONVECTION UNDER PURE VAPOR . . . . . . . . . . . . . 88

4.1 Fluid Flow and Temperature Fields . . . . . . . . . . . . . . . . . . . . . 89

4.2 Theoretical Analysis . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 92

4.2.1 Interfacial Temperature . . . . . . . . . . . . . . . . . . . . . . . 92

4.2.2 Thermal Boundary Layer Thickness . . . . . . . . . . . . . . . . 97

4.2.3 Interfacial Flow Speed . . . . . . . . . . . . . . . . . . . . . . . 98

4.2.4 Newton's Law of Cooling . . . . . . . . . . . . . . . . . . . . . . 99

4.3 Comparison of Different Phase Change Models . . . . . . . . . . . . . . 101

4.4 Dependence on the Accommodation Coeffcient . . . . . . . . . . . . . . 105

4.5 Disc

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: 16979.00 р.
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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.


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