Progress in Aircraft Engines Materials and Their Properties
Abstract
This chapter explores the development of materials in aircraft engines in terms of performance, safety, and efficiency improvements that characterizes modern aviation. This chapter follows the historical development and the current status of aircraft engine materials from the early 20th-century dependence on wood, steel, and aluminum to the present high-performance alloys and composites. It highlights the severe requirements imposed on aircraft engines, like mechanical loads and corrosive atmospheres, as well as extreme temperatures and the resultant requirement for higher-performance materials like titanium and nickel-based superalloys, ceramic matrix composites (CMCs), and carbon–carbon composites. These materials exhibit high strength-to-weight ratios, thermal resistance, and durability under stress. The chapter also addresses particular materials for specific engine components and the importance of protective coatings in increasing component lifespan. It also highlights the shift to cleaner, lighter, and more efficient designs due to increasing environmental and economic pressures. With the help of advanced manufacturing processes and material advancements, aircraft engines now have higher thrust-to-weight ratios, better fuel efficiency, and longer operational lifespans, defining the future of aerospace propulsion.
Fields of Study & Subjects
Material Properties and Applications
High Temperature Alloys and Creep
Material Selection and Properties
Publication details
- Journal / source
- CRC Press eBooks
- Pages
- 40–56
- Publication date
- 12 February 2026
- Language
- EN
- Document type
- Book chapter