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  • Kunyuan Zhang
    978-981-15-0727-4
    2020
    Edition 1
    • Introduces curved shock wave-curved compression surface applied to the compression surface design of supersonic velocity–hypersonic inlet
    • Provides results that can be adopted in the aerodynamic design of hypersonic airbreathing engines
    • Proposes aerodynamic configuration of inlet with excellent performance
    €418 €376
    10% OFF

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