Name: Scramjets: Fuel Mixing and Injection Systems (en Inglés)
Price: 186620.00 CLP
Availability: InStock
Author: Mostafa Barzegar Gerdroodbary
ISBN: 9780128211380

portada Scramjets: Fuel Mixing and Injection Systems (en Inglés)

Formato

Libro Físico

Editorial

Butterworth Heinemann

Autor

Mostafa Barzegar Gerdroodbary

Año

2020

Idioma

Inglés

N° páginas

228

Encuadernación

Tapa Blanda

ISBN13

9780128211380

Categorías

Tecnología aeroespacial y aeronáutica
Astronáutica

Scramjets: Fuel Mixing and Injection Systems (en Inglés)

Mostafa Barzegar Gerdroodbary (Autor) · Butterworth Heinemann · Tapa Blanda

Libro Físico

$ 186.620

$ 311.030

Ahorras: $ 124.410

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Envío normal

Origen: Reino Unido (Costos de importación incluídos en el precio)

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Reseña del libro "Scramjets: Fuel Mixing and Injection Systems (en Inglés)"

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.