Overview
- Authors:
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Tuncer Cebeci
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Douglas Aircraft Company, Long Beach, USA
Department of Mechanical Engineering, California State University, Long Beach, Long Beach, USA
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Peter Bradshaw
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Department of Aeronautics, Imperial College of Science and Technology, London, England
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Table of contents (14 chapters)
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- Tuncer Cebeci, Peter Bradshaw
Pages 1-18
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- Tuncer Cebeci, Peter Bradshaw
Pages 19-40
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- Tuncer Cebeci, Peter Bradshaw
Pages 41-70
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- Tuncer Cebeci, Peter Bradshaw
Pages 71-123
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- Tuncer Cebeci, Peter Bradshaw
Pages 124-149
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- Tuncer Cebeci, Peter Bradshaw
Pages 150-215
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- Tuncer Cebeci, Peter Bradshaw
Pages 216-237
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- Tuncer Cebeci, Peter Bradshaw
Pages 238-262
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- Tuncer Cebeci, Peter Bradshaw
Pages 263-300
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- Tuncer Cebeci, Peter Bradshaw
Pages 301-332
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- Tuncer Cebeci, Peter Bradshaw
Pages 333-371
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- Tuncer Cebeci, Peter Bradshaw
Pages 372-384
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- Tuncer Cebeci, Peter Bradshaw
Pages 385-428
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- Tuncer Cebeci, Peter Bradshaw
Pages 429-455
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Back Matter
Pages 456-487
About this book
This volume is concerned with the transport of thermal energy in flows of practical significance. The temperature distributions which result from convective heat transfer, in contrast to those associated with radiation heat transfer and conduction in solids, are related to velocity characteristics and we have included sufficient information of momentum transfer to make the book self-contained. This is readily achieved because of the close relation ship between the equations which represent conservation of momentum and energy: it is very desirable since convective heat transfer involves flows with large temperature differences, where the equations are coupled through an equation of state, as well as flows with small temperature differences where the energy equation is dependent on the momentum equation but the momentum equation is assumed independent of the energy equation. The equations which represent the conservation of scalar properties, including thermal energy, species concentration and particle number density can be identical in form and solutions obtained in terms of one dependent variable can represent those of another. Thus, although the discussion and arguments of this book are expressed in terms of heat transfer, they are relevant to problems of mass and particle transport. Care is required, however, in making use of these analogies since, for example, identical boundary conditions are not usually achieved in practice and mass transfer can involve more than one dependent variable.
Authors and Affiliations
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Douglas Aircraft Company, Long Beach, USA
Tuncer Cebeci
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Department of Mechanical Engineering, California State University, Long Beach, Long Beach, USA
Tuncer Cebeci
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Department of Aeronautics, Imperial College of Science and Technology, London, England
Peter Bradshaw
