Name: High-Speed Airfoil Aerodynamics: Supersonic Laminar Boundary Insights: From Advanced Modeling and Computational Simulations to Experimental Validation (en Inglés)
SKU: 63929715
Price: 1450.94 MXN
Availability: InStock
Author: Nasser Eddegdag; Mohammed Radouani; Aze-Eddine Naamane
ISBN: 9786208416478

portada High-Speed Airfoil Aerodynamics: Supersonic Laminar Boundary Insights: From Advanced Modeling and Computational Simulations to Experimental Validation (en Inglés)

High-Speed Airfoil Aerodynamics: Supersonic Laminar Boundary Insights: From Advanced Modeling and Computational Simulations to Experimental Validation (en Inglés)

Formato

Libro Físico

Editorial

Lap Lambert Academic Publishing

Autor

Nasser Eddegdag; Mohammed Radouani; Aze-Eddine Naamane

Idioma

Inglés

N° páginas

192

Encuadernación

Tapa Blanda

ISBN13

9786208416478

High-Speed Airfoil Aerodynamics: Supersonic Laminar Boundary Insights: From Advanced Modeling and Computational Simulations to Experimental Validation (en Inglés)

Nasser Eddegdag; Mohammed Radouani; Aze-Eddine Naamane (Autor) · Lap Lambert Academic Publishing · Tapa Blanda

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Reseña del libro "High-Speed Airfoil Aerodynamics: Supersonic Laminar Boundary Insights: From Advanced Modeling and Computational Simulations to Experimental Validation (en Inglés)"

This book rigorously examines supersonic laminar boundary layer dynamics around thin airfoils, aiming for breakthroughs in aerodynamic efficiency and fuel savings in high-speed aerospace applications. By integrating analytical modeling, computational simulations, and experimental validation, this research refines traditional supersonic flow models. Employing advanced boundary layer theory and introducing a local linkage Mach number m, the model captures critical interactions such as shock waves, compressibility effects, and adverse pressure gradients with remarkable accuracy. The model's precision is confirmed through high-fidelity Ansys Fluent simulations and experimental AF300 wind tunnel tests on NACA airfoils, achieving accuracies within 3% for drag and 5% for lift. These results not only validate the model's robustness but also set a new standard for high-speed aerodynamics, offering a pathway for optimized airfoil design in civil and military applications. This foundational work supports future exploration into flow hybrid control techniques, promising to revolutionize maneuverability and efficiency in supersonic flight in civil and military aviation.