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This successful book gives an introduction to the basics of aerothermodynamics, as applied in particular to winged re-entry vehicles and airbreathing hypersonic cruise and acceleration vehicles. The book gives a review of the issues of transport of momentum, energy and mass, real-gas effects as well as inviscid and viscous flow phenomena. In this second, revised edition the chapters with the classical topics of aerothermodynamics more or less were left untouched. The access to some single topics of practical interest was improved. Auxiliary chapters were put into an appendix. The recent successful flights of the X-43A and the X-51A indicate that the dawn of sustained airbreathing hypersonic flight now has arrived. This proves that the original approach of the book to put emphasis on viscous effects and the aerothermodynamics of radiation-cooled vehicle surfaces was timely. This second, revised edition even more accentuates these topics. A new, additional chapter treats examples of viscous thermal surface effects. Partly only very recently obtained experimental and numerical results show the complexity of such phenomena (dependence of boundary-layer stability, skin friction, boundary-layer thicknesses, and separation on the thermal state of the surface) and their importance for airbreathing hypersonic flight vehicles, but also for any other kind of hypersonic vehicle.
Engineering. --- Aerospace Technology and Astronautics. --- Fluid- and Aerodynamics. --- Engineering Thermodynamics, Heat and Mass Transfer. --- Engineering Fluid Dynamics. --- Vibration, Dynamical Systems, Control. --- Thermodynamics. --- Vibration. --- Hydraulic engineering. --- Astronautics. --- Ingénierie --- Thermodynamique --- Vibration --- Technologie hydraulique --- Astronautique --- Mechanical Engineering --- Engineering & Applied Sciences --- Aeronautics Engineering & Astronautics --- Aerothermodynamics. --- Aerodynamics, Hypersonic. --- Aerodynamics of hypersonic flight --- Hypersonic aerodynamics --- Hypersonic speeds --- Hypersonics --- Thermoaerodynamics --- Fluids. --- Heat engineering. --- Heat transfer. --- Mass transfer. --- Dynamical systems. --- Dynamics. --- Fluid mechanics. --- Aerospace engineering. --- Aerodynamics, Supersonic --- Mach number --- Sound pressure --- Aerodynamics, Transonic --- Astronautics --- High-speed aeronautics --- Thermodynamics --- Chemistry, Physical and theoretical --- Dynamics --- Mechanics --- Physics --- Heat --- Heat-engines --- Quantum theory --- Cycles --- Sound --- Engineering, Hydraulic --- Engineering --- Fluid mechanics --- Hydraulics --- Shore protection --- Construction --- Industrial arts --- Technology --- Space sciences --- Aeronautics --- Astrodynamics --- Space flight --- Space vehicles --- Dynamical systems --- Kinetics --- Mathematics --- Mechanics, Analytic --- Force and energy --- Statics --- Hydromechanics --- Continuum mechanics --- Mass transport (Physics) --- Transport theory --- Heat transfer --- Thermal transfer --- Transmission of heat --- Energy transfer --- Mechanical engineering --- Hydrostatics --- Permeability --- Aeronautical engineering
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This book gives an introduction to the basics of aerothermodynamics, as applied in particular to winged re-entry vehicles and airbreathing cruise and acceleration vehicles. Beginning with a broad vehicle classification and a discussion of the flight environment, Basics of Aero-thermodynamics focuses on flight in the earth's atmosphere at speeds below approximately 8.0 km/s at altitudes below approximately 100.0 km. At such flight conditions the outer surfaces of hypersonic flight vehicles primarily are radiation cooled. This is taken into account by an introduction to the problem of the thermal state of the surface, and especially to the phenomena connected with surface radiation cooling. These are themes, which reappear throughout the remaining chapters. The implications of radiation cooling are different for the different vehicle classes. In any case the properties of both attached viscous and separating flows as well as thermo-chemical effects at and near the vehicle surface need to be considered. After a review of the issues of transport of momentum, energy and mass, real-gas effects as well as inviscid and viscous flow phenomena are treated. In view of their special importance for airbreathing hypersonic flight vehicles and for the discrete numerical methods of aerothermodynamics, considerable discussion is devoted to the issues of laminar-turbulent transition and turbulence, which follows a treatment of strong-interaction phenomena. Finally, simulation techniques for aerothermodynamics are considered, including computational methods and their modelling problems, as well as the problems of ground facility and in-flight simulation, including the hot experimental technique. The implications of Oswatitsch's Mach number independence principle are also treated. The book is for graduate students, doctoral students, design and development engineers, but also for technical managers. The reader should be familiar with the basics of fluid mechanics, aerodynamics, and thermodynamics.
Aerothermodynamics. --- Aerodynamics, Hypersonic. --- Aérothermodynamique --- Aérodynamique hypersonique --- Aerothermodynamics --- Aerodynamics, Hypersonic --- Mechanical Engineering --- Engineering & Applied Sciences --- Aeronautics Engineering & Astronautics --- Automotive Engineering --- High-speed aeronautics. --- Hypersonic planes. --- Aérothermodynamique --- Aérodynamique hypersonique --- EPUB-LIV-FT LIVINGEN SPRINGER-B --- Aeronautics, High-speed --- High-speed flight --- Supersonic aeronautics --- Hypersonic aircraft --- Planes, Hypersonic --- Thermoaerodynamics --- Engineering. --- Computational intelligence. --- Thermodynamics. --- Heat engineering. --- Heat transfer. --- Mass transfer. --- Continuum mechanics. --- Fluid mechanics. --- Automotive engineering. --- Automotive Engineering. --- Computational Intelligence. --- Engineering, general. --- Engineering Thermodynamics, Heat and Mass Transfer. --- Continuum Mechanics and Mechanics of Materials. --- Engineering Fluid Dynamics. --- Hydromechanics --- Continuum mechanics --- Mechanics of continua --- Elasticity --- Mechanics, Analytic --- Field theory (Physics) --- Mass transport (Physics) --- Thermodynamics --- Transport theory --- Heat transfer --- Thermal transfer --- Transmission of heat --- Energy transfer --- Heat --- Mechanical engineering --- Chemistry, Physical and theoretical --- Dynamics --- Mechanics --- Physics --- Heat-engines --- Quantum theory --- Intelligence, Computational --- Artificial intelligence --- Soft computing --- Construction --- Industrial arts --- Technology --- Airplanes --- High-speed aeronautics --- Aeronautics --- Aerodynamics, Supersonic --- Aerodynamics, Transonic --- Astronautics --- Mechanics. --- Mechanics, Applied. --- Hydraulic engineering. --- Solid Mechanics. --- Engineering, Hydraulic --- Engineering --- Fluid mechanics --- Hydraulics --- Shore protection --- Applied mechanics --- Engineering, Mechanical --- Engineering mathematics --- Classical mechanics --- Newtonian mechanics
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Fluid mechanical aspects of separated and vortical flow in aircraft wing aerodynamics are treated. The focus is on two wing classes: (1) large aspect-ratio wings and (2) small aspect-ratio delta-type wings. Aerodynamic design issues in general are not dealt with. Discrete numerical simulation methods play a progressively larger role in aircraft design and development. Accordingly, in the introduction to the book the different mathematical models are considered, which underlie the aerodynamic computation methods (panel methods, RANS and scale-resolving methods). Special methods are the Euler methods, which as rather inexpensive methods embrace compressibility effects and also permit to describe lifting-wing flow. The concept of the kinematically active and inactive vorticity content of shear layers gives insight into many flow phenomena, but also, with the second break of symmetry---the first one is due to the Kutta condition---an explanation of lifting-wing flow fields. The prerequisite is an extended definition of separation: “flow-off separation” at sharp trailing edges of class (1) wings and at sharp leading edges of class (2) wings. The vorticity-content concept, with a compatibility condition for flow-off separation at sharp edges, permits to understand the properties of the evolving trailing vortex layer and the resulting pair of trailing vortices of class (1) wings. The concept also shows that Euler methods at sharp delta or strake leading edges of class (2) wings can give reliable results. Three main topics are treated: 1) Basic Principles are considered first: boundary-layer flow, vortex theory, the vorticity content of shear layers, Euler solutions for lifting wings, the Kutta condition in reality and the topology of skin-friction and velocity fields. 2) Unit Problems treat isolated flow phenomena of the two wing classes. Capabilities of panel and Euler methods are investigated. One Unit Problem is the flow past the wing of the NASA Common Research Model. Other Unit Problems concern the lee-side vortex system appearing at the Vortex-Flow Experiment 1 and 2 sharp- and blunt-edged delta configurations, at a delta wing with partly round leading edges, and also at the Blunt Delta Wing at hypersonic speed. 3) Selected Flow Problems of the two wing classes. In short sections practical design problems are discussed. The treatment of flow past fuselages, although desirable, was not possible in the frame of this book.
Fluid mechanics. --- Computational intelligence. --- Engineering Fluid Dynamics. --- Computational Intelligence. --- Intelligence, Computational --- Artificial intelligence --- Soft computing --- Hydromechanics --- Continuum mechanics --- Engineering --- Fluid Dynamics. --- Industrial arts --- Technology --- Construction
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This successful book gives an introduction to the basics of aerothermodynamics, as applied in particular to winged re-entry vehicles and airbreathing hypersonic cruise and acceleration vehicles. The book gives a review of the issues of transport of momentum, energy and mass, real-gas effects as well as inviscid and viscous flow phenomena. In this second, revised edition the chapters with the classical topics of aerothermodynamics more or less were left untouched. The access to some single topics of practical interest was improved. Auxiliary chapters were put into an appendix. The recent successful flights of the X-43A and the X-51A indicate that the dawn of sustained airbreathing hypersonic flight now has arrived. This proves that the original approach of the book to put emphasis on viscous effects and the aerothermodynamics of radiation-cooled vehicle surfaces was timely. This second, revised edition even more accentuates these topics. A new, additional chapter treats examples of viscous thermal surface effects. Partly only very recently obtained experimental and numerical results show the complexity of such phenomena (dependence of boundary-layer stability, skin friction, boundary-layer thicknesses, and separation on the thermal state of the surface) and their importance for airbreathing hypersonic flight vehicles, but also for any other kind of hypersonic vehicle.
Mathematics --- Space research --- Astronomy --- Classical mechanics. Field theory --- Fluid mechanics --- Thermodynamics --- Mechanical properties of solids --- Materials sciences --- Heat engines. Steam engines --- Gases handling. Fluids handling --- Applied physical engineering --- Engineering sciences. Technology --- Air traffic --- Fuels --- patroonherkenning --- vloeistofstroming --- thermodynamica --- aerodynamica --- astronauten --- engineering --- luchtvaart --- ingenieurswetenschappen --- fysica --- ruimtevaart --- dynamica --- vloeistoffen --- warmteoverdracht --- optica
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Fluid mechanics --- Numerical analysis --- Approximation methods
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This volume contains 37 invited contributions, collected to celebrate one hundred volumes of the NNFM Series. After a general introduction overviews are given in five parts of the developments in numerical fluid mechanics and related fields. In the first part information about the series is given, its origins are discussed, as well as its environment and the German and European high-performance computer scene. In Part II the co-editors of the series give short surveys over developments in their countries. Current applications, mainly in the aerospace sector, but also in the automotive sector, are discussed in Part III. Applications to flow problems in engineering and physics, ranging from hydraulic machinery to astrophysics, are the topics of Part IV. Algorithms, computer science, commercial CFD, public partnerships in high-performance computing, and hardware development up to petaflops computers are treated in Part V. All volumes, which were published in the series finally are listed in Part VI.
Aerodynamics --Mathematical models. --- Fluid mechanics --Mathematical models. --- Fluid mechanics --- Aerodynamics --- Civil & Environmental Engineering --- Engineering & Applied Sciences --- Civil Engineering --- Applied Mathematics --- Mathematical models --- Mathematical models. --- Hydromechanics --- Engineering. --- Computer simulation. --- Computer mathematics. --- Physics. --- Fluids. --- Computational intelligence. --- Fluid mechanics. --- Engineering Fluid Dynamics. --- Fluid- and Aerodynamics. --- Simulation and Modeling. --- Computational Mathematics and Numerical Analysis. --- Computational Intelligence. --- Numerical and Computational Physics. --- Continuum mechanics --- Intelligence, Computational --- Artificial intelligence --- Soft computing --- Hydraulics --- Mechanics --- Physics --- Hydrostatics --- Permeability --- Natural philosophy --- Philosophy, Natural --- Physical sciences --- Dynamics --- Computer mathematics --- Discrete mathematics --- Electronic data processing --- Computer modeling --- Computer models --- Modeling, Computer --- Models, Computer --- Simulation, Computer --- Electromechanical analogies --- Simulation methods --- Model-integrated computing --- Construction --- Industrial arts --- Technology --- Mathematics --- Hydraulic engineering. --- Computer science --- Numerical and Computational Physics, Simulation. --- Mathematics. --- Engineering, Hydraulic --- Engineering --- Shore protection --- Continuum mechanics. --- Mathematical physics. --- Continuum Mechanics. --- Computer Modelling. --- Theoretical, Mathematical and Computational Physics. --- Data processing. --- Physical mathematics --- Mechanics of continua --- Elasticity --- Mechanics, Analytic --- Field theory (Physics)
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This volume addresses selected aerothermodynamic design problems for three vehicle classes: winged reentry, non-winged reentry, and airbreathing hypersonic flight vehicles. Following an introductory chapter, the book presents the basics of flight trajectory mechanics, giving the aerothermodynamicist an understanding of the principal issues relevant to the field. In the following chapters, specific aerothermodynamic phenomena are discussed for the three vehicle classes, major simulation problems are singled out, and particular trends are examined. Available coefficients of longitudinal motion are presented for a variety of shapes of operational and studied vehicles, and aerothermodynamic issues of stabilization, trim, and control devices are treated. A full chapter is devoted to describing equations for aerodynamic forces, moments, center of pressure, trim, and stability. Another chapter focuses on multidisciplinary design aspects, presenting the mathematical models and the coupling procedures in detail. Other chapters address the thermal state of a vehicle surface, thermal loads, and thermal surface effects, which are among the major topics of hypersonic vehicle design. The governing equations for flow in thermo-chemical non-equilibrium are presented, along with properties of the earth’s atmosphere. Finally, constants and dimensions, symbol definitions, a glossary, acronyms, and a solution guide to problems are provided. This book will be a great boon to graduate students, doctoral students, design and development engineers, and technical managers alike.
Aerodynamics, Hypersonic. --- Aerothermodynamics. --- Hypersonic planes -- Design and construction. --- Aerothermodynamics --- Aerodynamics, Hypersonic --- Hypersonic planes --- Mechanical Engineering --- Aeronautics Engineering & Astronautics --- Automotive Engineering --- Engineering & Applied Sciences --- Design and construction --- Design and construction. --- Hypersonic aircraft --- Planes, Hypersonic --- Aerodynamics of hypersonic flight --- Hypersonic aerodynamics --- Hypersonic speeds --- Hypersonics --- Thermoaerodynamics --- Engineering. --- Computational intelligence. --- Automotive engineering. --- Automotive Engineering. --- Computational Intelligence. --- Intelligence, Computational --- Artificial intelligence --- Soft computing --- Construction --- Industrial arts --- Technology --- Airplanes --- High-speed aeronautics --- Aerodynamics, Supersonic --- Mach number --- Sound pressure --- Aerodynamics, Transonic --- Astronautics --- Thermodynamics
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Viscous flow is usually treated in the frame of boundary-layer theory and as a two-dimensional flow. At best, books on boundary layers provide the describing equations for three-dimensional boundary layers, and solutions only for certain special cases. This book presents the basic principles and theoretical foundations of three-dimensional attached viscous flows as they apply to aircraft of all kinds. Though the primary flight speed range is that of civil air transport vehicles, flows past other flying vehicles up to hypersonic speeds are also considered. Emphasis is put on general three-dimensional attached viscous flows and not on three-dimensional boundary layers, as this wider scope is necessary in view of the theoretical and practical problems that have to be overcome in practice. The specific topics covered include weak, strong, and global interaction; the locality principle; properties of three-dimensional viscous flows; thermal surface effects; characteristic properties; wall compatibility conditions; connections between inviscid and viscous flows; flow topology; quasi-one- and two-dimensional flows; laminar-turbulent transition; and turbulence. Detailed discussions of examples illustrate these topics and the relevant phenomena encountered in three-dimensional viscous flows. The full governing equations, reference-temperature relations for qualitative considerations and estimations of flow properties, and coordinates for fuselages and wings are also provided. Sample problems with solutions allow readers to test their understanding. .
Viscous flow. --- Fluid dynamics. --- Engineering. --- Fluids. --- Thermodynamics. --- Heat engineering. --- Heat transfer. --- Mass transfer. --- Fluid mechanics. --- Aerospace engineering. --- Astronautics. --- Aerospace Technology and Astronautics. --- Engineering Fluid Dynamics. --- Fluid- and Aerodynamics. --- Engineering Thermodynamics, Heat and Mass Transfer. --- Dynamics --- Fluid mechanics --- Fluid dynamics --- Viscosity --- Hydraulic engineering. --- Construction --- Industrial arts --- Technology --- Space sciences --- Aeronautics --- Astrodynamics --- Space flight --- Space vehicles --- Engineering, Hydraulic --- Engineering --- Hydraulics --- Shore protection --- Hydromechanics --- Continuum mechanics --- Aeronautical engineering --- Astronautics --- Mass transport (Physics) --- Thermodynamics --- Transport theory --- Heat transfer --- Thermal transfer --- Transmission of heat --- Energy transfer --- Heat --- Mechanical engineering --- Chemistry, Physical and theoretical --- Mechanics --- Physics --- Heat-engines --- Quantum theory --- Hydrostatics --- Permeability
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