Advertisement

Fundamentals of Aircraft and Rocket Propulsion

  • Ahmed F. El-Sayed

Table of contents

  1. Front Matter
    Pages i-xxi
  2. Ahmed F. El-Sayed
    Pages 91-160
  3. Ahmed F. El-Sayed
    Pages 161-218
  4. Ahmed F. El-Sayed
    Pages 219-314
  5. Ahmed F. El-Sayed
    Pages 315-401
  6. Ahmed F. El-Sayed
    Pages 531-588
  7. Ahmed F. El-Sayed
    Pages 589-701
  8. Ahmed F. El-Sayed
    Pages 703-838
  9. Ahmed F. El-Sayed
    Pages 839-905
  10. Ahmed F. El-Sayed
    Pages 907-991
  11. Back Matter
    Pages 993-1010

About this book

Introduction

This book provides a comprehensive basics-to-advanced course in an aero-thermal science vital to the design of engines for either type of craft. The text classifies engines powering aircraft and single/multi-stage rockets, and derives performance parameters for both from basic aerodynamics and thermodynamics laws. Each type of engine is analyzed for optimum performance goals, and mission-appropriate engines selection is explained.

Fundamentals of Aircraft and Rocket Propulsion provides information about and analyses of:

  • thermodynamic cycles of shaft engines (piston, turboprop, turboshaft and propfan);
  • jet engines (pulsejet, pulse detonation engine, ramjet, scramjet, turbojet and turbofan);
  • chemical and non-chemical rocket engines;
  • conceptual design of modular rocket engines (combustor, nozzle and turbopumps); and
  • conceptual design of different modules of aero-engines in their design and off-design state.

Aimed at graduate and final-year undergraduate students, this textbook provides a thorough grounding in the history and classification of both aircraft and rocket engines, important design features of all the engines detailed, and particular consideration of special aircraft such as unmanned aerial and short/vertical takeoff and landing aircraft. End-of-chapter exercises make this a valuable student resource, and the provision of a downloadable solutions manual will be of further benefit for course instructors.

Keywords

Aircraft Propulsion Aircraft Engines Future Design Trends in Aerospace Rocket Propulsion Contra-rotating turbine

Authors and affiliations

  • Ahmed F. El-Sayed
    • 1
  1. 1.Dept of Mechanical EngineeringZagazig UniversityZagazigEgypt

Bibliographic information

  • DOI https://doi.org/10.1007/978-1-4471-6796-9
  • Copyright Information Springer-Verlag London 2016
  • Publisher Name Springer, London
  • eBook Packages Engineering
  • Print ISBN 978-1-4471-6794-5
  • Online ISBN 978-1-4471-6796-9
  • Buy this book on publisher's site