Heat transfer in aero-engines

Author: Cao Yuzhang
Publisher:
Publish Date: 2005-04-01
Features: This book focuses on the heat transfer of aviation gas turbine engines, introducing the working principles and calculation methods of various cooling methods and waterproof measures in aviation gas turbine engines. It also provides a systematic introduction to the heat transfer characteristics and cooling structures of various hot-end components in the engine. The book consists of 10 chapters: Chapter 1 serves as an introduction, providing an overall overview of heat transfer in aviation gas turbine engines; Chapters 3, 4, and 5 introduce the principles and calculations of divergent cooling, film cooling, and impingement cooling; Chapters 2, 6, 7, and 8 cover the heat transfer calculations of hot-end components; Chapter 9 discusses the calculation of the engine's air (cooling) system; and Chapter 10 introduces experimental research techniques for aviation engine heat transfer. This book can be used as a textbook for undergraduate and graduate students in relevant fields at universities and colleges, as well as a reference for aviation engine designers.