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. 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.

-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

- Focusses on intricate aspects of cowl design and throat shaping

- Explores buzz simulation using a simplified analytical model, providing valuable insights into the complex dynamics of supersonic intakes

This book is aimed at graduate students, researchers and professionals in aircraft propulsion, intake design, and aerospace engineering.