Abstract
This chapter is the core of this book. It introduces the detailed process of the second class inverse design, i.e., to design the molded surface of the compression surface and the whole compression flow field with specified pressure distribution of the compression surface wall; or specify the deceleration law of the compression surface to design the geometric molded surface of the compression surface and complete curved shock wave compression flow field. This is a very practical design method, by which a practical inlet of good performance can be designed. This design method has been applied in the practical engineering and has achieved good results.
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References
Wang L (2016) Analysis, optimization and application of hypersonic quadratic curved shock wave compression flow field. Doctoral dissertation, Nanjing University of Aeronautics & Astronautics
Zhang L (2014) Study on the supersonic/hypersonic curved compression system with dispersed intersection of isentropic compression wave. Doctoral dissertation, Nanjing University of Aeronautics & Astronautic
Li YZ (2014) Study on the hypersonic internal contraction inlet with controllable Mach number distribution and its integrated design. Doctoral dissertation, Nanjing University of Aeronautics & Astronautics
Nan XJ (2012) Study on the design method of hypersonic internal contraction inlet with controllable pressure rising rule. Doctoral dissertation, Nanjing University of Aeronautics & Astronautics
Liu CH (2014) A preliminary study of the hypersonic sidewall compression inlet with controllable wall parameter fusion. Master’s dissertation, Nanjing University of Aeronautics & Astronautics
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© 2020 Zhejiang University Press and Springer Nature Singapore Pte Ltd.
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Zhang, K. (2020). Inverse Design of Curved Shock Wave Compression Surface on Basis of Specified Wall Aerodynamic Parameters. In: Hypersonic Curved Compression Inlet and Its Inverse Design. Advanced Topics in Science and Technology in China, vol 56. Springer, Singapore. https://doi.org/10.1007/978-981-15-0727-4_5
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DOI: https://doi.org/10.1007/978-981-15-0727-4_5
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Online ISBN: 978-981-15-0727-4
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