Fundamentals of Aircraft and Rocket Propulsion

Fundamentals of Aircraft and Rocket Propulsion is a textbook that covers the basics to advanced aero-thermal science for designing engines for aircraft and single/multi-stage rockets. It analyzes each type of engine for optimum performance goals and mission-appropriate engines selection. It is aimed at graduate and final-year undergraduate students and provides a thorough grounding in the history and classification of both aircraft and rocket engines, important design features, and special aircraft.

Format: Paperback / softback
Length: 1010 pages
Publication date: 26 May 2018
Publisher: Springer London Ltd

This comprehensive textbook offers a thorough and in-depth exploration of the essential principles and applications of aero-thermal science, providing a vital foundation for the design of engines for both aircraft and rockets. It meticulously categorizes engines powering aircraft and single/multi-stage rockets, drawing upon fundamental aerodynamics and thermodynamics laws to derive performance parameters for each. The text then conducts a detailed analysis of each type of engine, aiming to optimize its performance for specific mission requirements.

Furthermore, it delves into the conceptual design of modular rocket engines, encompassing the combustor, nozzle, and turbopumps. Additionally, the book provides a comprehensive overview of the history and classification of both aircraft and rocket engines, highlighting important design features and considering the unique requirements of special aircraft such as unmanned aerial vehicles and short/vertical takeoff and landing aircraft.

To enhance the learning experience, the textbook includes a range of end-of-chapter exercises that reinforce key concepts and encourage students to apply their knowledge. This makes Fundamentals of Aircraft and Rocket Propulsion an invaluable resource for graduate and final-year undergraduate students seeking to gain a deep understanding of this critical field.

In summary, this textbook serves as a indispensable guide for anyone interested in the design and development of engines for aircraft and rockets, offering a comprehensive and up-to-date understanding of the principles and practices of aero-thermal science.

Weight: 1916g
Dimension: 157 x 235 x 52 (mm)
ISBN-13: 9781447173939
Edition number: Softcover reprint of the original 1st ed. 2016