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Hypersonic Curved Compression Inlet and Its Inverse Design

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Attention for Chapter 6: Inverse Design of Axisymmetric Basic Flow Field on Basis of Specified Wall Aerodynamic Parameters
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Chapter title
Inverse Design of Axisymmetric Basic Flow Field on Basis of Specified Wall Aerodynamic Parameters
Chapter number 6
Book title
Hypersonic Curved Compression Inlet and Its Inverse Design
Published by
Springer, Singapore, January 2020
DOI 10.1007/978-981-15-0727-4_6
Book ISBNs
978-9-81-150726-7, 978-9-81-150727-4
Authors

Kunyuan Zhang