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  • Format: ePub

Scramjet engines are a type of jet engine and rely on the combustion of fuel and an oxidizer to produce thrust. While scramjets are conceptually simple, actual implementation is limited by extreme technical challenges. Hypersonic flight within the atmosphere generates immense drag, and temperatures found on the aircraft and within the engine can be much greater than that of the surrounding air. Maintaining combustion in the supersonic flow presents additional challenges, as the fuel must be injected, mixed, ignited, and burned within milliseconds. Fuel mixing, along with the configuration and…mehr

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Produktbeschreibung
Scramjet engines are a type of jet engine and rely on the combustion of fuel and an oxidizer to produce thrust. While scramjets are conceptually simple, actual implementation is limited by extreme technical challenges. Hypersonic flight within the atmosphere generates immense drag, and temperatures found on the aircraft and within the engine can be much greater than that of the surrounding air. Maintaining combustion in the supersonic flow presents additional challenges, as the fuel must be injected, mixed, ignited, and burned within milliseconds. Fuel mixing, along with the configuration and positioning of the injectors and the boundary conditions, play a key role in combustion efficiency.



Scramjets: Fuel Mixing and Injection Systems
discusses how fuel mixing efficiency and the advantage of injection systems can enhance the performance of the scramjets. The book begins with the introduction of the supersonic combustion chamber and explains the main parameters on the mixing rate. The configuration of scramjets is then introduced with special emphasis on the main effective parameters on the mixing of fuel inside the scramjets. In addition, basic concepts and principles on the mixing rate and fuel distribution within scramjets are presented. Main effective parameters such as range of fuel concentration for the efficient combustion, pressure of fuel jet and various arrangement of jet injections are also explained. This book is for aeronautical and mechanical engineers as well as those working in supersonic combustion who need to know the effects of compressibility on combustion, of shocks on mixing and on chemical reactions, and vorticity on the flame anchoring.

  • Explains the main applicable approaches for enhancement of supersonic combustion engines and the new techniques of fuel injection
  • Shows how the interaction of main air stream with fuel injections can develop the mixing inside the scramjets
  • Presents results of numerical simulations and how they can be used for the development of the combustion engines

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Autorenporträt
Dr. Mostafa Barzegar Gerdroodbary is a Research Associate at Babol Noshirvani University of Technology. He obtained his Ph.D. in Mechanical Engineering at Babol Noshirvani University of Technology, IRAN in 2019. He completed his Ph.D. on modelling of rarefied gas flow for calibration of gas sensor using DSMC. He published two authored books (Scramjets: fuel mixing and injection systems, Aerodynamic Heating in Supersonic and Hypersonic Flows) and two book chapters (Gas Sensors, Nanotechnology for Light Pollution Reduction) and more than 70 journal articles in high rank journals. For his outstanding research, Dr. Barzegar was included in the World's Top 2% Scientists 2021 list (by Stanford University). He is also a member of the editorial board for many journals such as Scientific Report.