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    Chapter and Conference Paper

    Measurement of Shock Wave Attenuation in a Micro-channel

    This work presents optical measurements of shock wave propagation in a glass micro-channel. This transparent facility, with a section ranging from 1 mm × 150 μm to 1 mm × 500 μm, exploits a high-speed schliere...

    J. Giordano, P. Perrier, L. Meister… in 31st International Symposium on Shock Wave… (2019)

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    Chapter

    Concepts of Hypersonic Aircraft

    Obviously, all concept of any aircraft is a compromise between conflicting requirements. Performance improvements generally induce direct cost.

    P. Perrier in Advances in Hypersonics (1992)