Titlebook: Hypersonic Curved Compression Inlet and Its Inverse Design; Kunyuan Zhang Book 2020 Zhejiang University Press and Springer Nature Singapor

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Introduction,lets are for turbojet engines or ramjet engines; the scope of working Mach number of hypersonic inlets determines the fact that they mainly serve scramjet engines or other combined cycle engines; therefore, the development of inlet is closely related to the history of development of aerospace dynamics.

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Introduction,lets are for turbojet engines or ramjet engines; the scope of working Mach number of hypersonic inlets determines the fact that they mainly serve scramjet engines or other combined cycle engines; therefore, the development of inlet is closely related to the history of development of aerospace dynami

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Calculation and Analysis Method of Two Dimensional Curved Shock Wave Curved Compression Flow Field,ntal aerodynamic phenomena. In this chapter, simplified calculation methods of basic aerodynamics problems, which are closely related to curved shock wave compression system, are introduced; a direct, accurate, highly efficient and simplified calculation method to avoid numerical iteration is provid

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Inverse Design of Compression Channel with Specified Exit Aerodynamic Parameters,rom the requirements of the outlet flow field; the second type is to design the molded line of compression surface from given distribution of aerodynamic parameters of the compression surface along the flow. In which the countercurrent design is the most challenging research work. In this chapter, w

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