Numerical Investigation and Performance Enhancement of Scramjet Inlets and Combustors (Paperback)

Sprache: Englisch

Verlag: Shark Nail, 2026

1962116743 / 9781962116749

Anbieter: Grand Eagle Retail, Bensenville, IL, USAGrand Eagle Retail

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Verkäufer:in bei AbeBooks seit 12. Oktober 2005

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Artikelbeschreibung des Verkäufers

Paperback. Scramjet propulsion relies on the efficient compression, mixing, and combustion of air flowing through an engine at very high speeds. The inlet and combustor are therefore critical components in determining the overall aerodynamic and combustion behavior of a scramjet system. Numerical Investigation and Performance Enhancement of Scramjet Inlets and Combustors provides a focused introduction to the computational analysis, aerodynamic behavior, combustion processes, and performance-enhancement concepts associated with scramjet propulsion.The book introduces the fundamental principles of air-breathing hypersonic propulsion and establishes the role of the scramjet inlet in decelerating and compressing incoming high-speed airflow while maintaining conditions suitable for supersonic combustion. Readers are introduced to concepts including compressible flow, Mach number, shock waves, boundary layers, pressure distribution, flow separation, and inlet performance. These foundations provide the necessary context for understanding the complex flow structures that develop within high-speed propulsion systems.A central focus is placed on numerical investigation of scramjet inlet and combustor performance. The text discusses computational approaches for analyzing high-speed compressible flow, including numerical modeling, computational fluid dynamics, flow-field prediction, pressure and temperature distributions, and performance assessment. The relationship between computational parameters, geometry, boundary conditions, and predicted aerodynamic behavior is considered within a general engineering framework.The book further examines scramjet inlet performance and methods for improving airflow characteristics. Topics such as shock-wave interactions, inlet compression, total pressure recovery, flow distortion, boundary-layer behavior, separation control, and mass-flow characteristics are considered in relation to inlet design. These concepts help readers understand the engineering trade-offs involved in developing inlet configurations capable of providing suitable flow conditions to the downstream combustor.Numerical Investigation and Performance Enhancement of Scramjet Inlets and Combustors explores computational methods for analyzing and improving scramjet propulsion components. Numerical Investigation and Performance Enhancement of Scramjet Inlets and Combustors explores computational methods for analyzing and improving scramjet propulsion components. This item is printed on demand. Shipping may be from multiple locations in the US or from the UK, depending on stock availability.…

Bestandsnummer des Verkäufers 9781962116749

Titel
Numerical Investigation and Performance Enhancement of Scramjet Inlets and Combustors (Paperback)
Autor
Kathy Bano
Verlag
Shark Nail
Erscheinungsjahr
2026
Zustand
new
Einband
Paperback
Sprache
Englisch
ISBN-10
1962116743
ISBN-13
9781962116749

Grand Eagle Retail

Bensenville, IL, USA

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Verkäufer:in bei AbeBooks seit 12. Oktober 2005

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