Heat Transfer in Aerospace Applications

Description

Heat Transfer in Aerospace Applications is the first book to provide an overall description of various heat transfer issues of relevance for aerospace applications. The book contains chapters relating to convection cooling, heat pipes, ablation, heat transfer at high velocity, low pressure and microgravity, aircraft heat exchangers, fuel cells, and cryogenic cooling systems. Chapters specific to low density heat transfer (4) and microgravity heat transfer (9) are newer subjects which have not been previously covered. The book takes a basic engineering approach by including correlations and examples that an engineer needs during the initial phases of vehicle design or to quickly analyze and solve a specific problem. Designed for mechanical, chemical, and aerospace engineers in research institutes, companies, and consulting firms, this book is an invaluable resource for the latest on aerospace heat transfer engineering and research. Content: Front Matter,Copyright,Preface,NomenclatureEntitled to full textChapter 1 - Introduction, Pages 1-17 Chapter 2 - Ablation, Pages 19-26 Chapter 3 - Aerodynamic Heating: Heat Transfer at High Speeds, Pages 27-44 Chapter 4 - Low-Density Heat Transfer: Rarefied Gas Heat Transfer, Pages 45-70 Chapter 5 - Cryogenics, Pages 71-88 Chapter 6 - Aerospace Heat Exchangers, Pages 89-115 Chapter 7 - Heat Pipes for Aerospace Application, Pages 117-144 Chapter 8 - Fuel Cells, Pages 145-153 Chapter 9 - Microgravity Heat Transfer, Pages 155-177 Chapter 10 - Computational Methods for the Investigations of Heat Transfer Phenomena in Aerospace Applications, Pages 179-196 Chapter 11 - Measuring Techniques, Pages 197-230 Appendix 1 - Governing Equations for Momentum, Mass, and Energy Transport, Pages 231-247 Appendix 2 - Dimensionless Numbers of Relevance in Aerospace Heat Transfer, Page 249 Index, Pages 251-255