Computational Design and Optimization of Supersonic Intakes
Uitgelicht
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140,42 |
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140,42 |
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149,00 |
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Beschrijving
Bol
This book offers a unique perspective of at the intersection supersonic intake design, formal optimization methods, and the use of computational fluid dynamics (CFD) for evaluating the performance of intakes. This book offers a unique perspective on the intersection of supersonic intake design, formal optimization methods, and the use of computational fluid dynamics (CFD) for evaluating the performance of intakes. Details of the meta-model and optimization scheme, as well the CFD solvers used at each stage of the optimization process, are presented. Additionally, for a balanced perspective, a separate chapter presents a faster, lower-fidelity alternative to RANS computation, complemented by its illustrative application to hypersonic intakes. Key Features: Discusses multi-objective design of supersonic intakes using formal optimization tools such as Kriging/MOGA. Leverages advancement in CFD methods and optimization techniques for practical supersonic intake design. Covers reduced-order analysis of supersonic intake. Focuses on the intricate aspects of cowl design and throat shaping. Presents conical intake design with geometric constraints and TPR-drag trade-offs This book is aimed at graduate students, researchers, and professionals in aircraft propulsion, intake design, and aerospace engineering.
This book offers a unique perspective of at the intersection supersonic intake design, formal optimization methods, and the use of computational fluid dynamics (CFD) for evaluating the performance of intakes. This book offers a unique perspective on the intersection of supersonic intake design, formal optimization methods, and the use of computational fluid dynamics (CFD) for evaluating the performance of intakes. Details of the meta-model and optimization scheme, as well the CFD solvers used at each stage of the optimization process, are presented. Additionally, for a balanced perspective, a separate chapter presents a faster, lower-fidelity alternative to RANS computation, complemented by its illustrative application to hypersonic intakes. Key Features: Discusses multi-objective design of supersonic intakes using formal optimization tools such as Kriging/MOGA. Leverages advancement in CFD methods and optimization techniques for practical supersonic intake design. Covers reduced-order analysis of supersonic intake. Focuses on the intricate aspects of cowl design and throat shaping. Presents conical intake design with geometric constraints and TPR-drag trade-offs This book is aimed at graduate students, researchers, and professionals in aircraft propulsion, intake design, and aerospace engineering.
AmazonPagina's: 174, Editie: Eerste editie, Hardcover, CRC Press