High-performance aviation gas turbine combustion technology

Author: Hou Xiaochun
Publisher:
Publish Date: 2002-01-01
Features: This book systematically and highlights the key points, introducing the latest scientific and technological achievements and development trends in combustion technology and testing technology of high-performance aviation gas turbine combustion chambers and afterburners. The book is divided into three parts, 19 chapters. The first part includes diffusers, fuel supply devices, efficient cooling methods, low-pollution combustion technology, and the development and application of computational combustion in short annular combustion chambers and small combustion chambers. The second part includes mixers/diffusers, ignition, fuel supply methods, thrust vector nozzles, and stealth technology in turbojet and turbofan afterburners, as well as numerical simulation calculations of ternary flow fields. The third part includes advanced measurement techniques for fuel atomization quality, exit temperature field divergence, combustion chamber life prediction, and special tests for afterburners. This book is mainly intended for university and college teachers and students majoring in gas turbines, as well as scientific and technical personnel engaged in combustion chamber and afterburner design and testing, and scientific and technical management personnel for reference.