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Introduction to Hypersonic Flows

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Abstract

In the previous chapters, compressibility effects are covered, particularly in the transonic regime where the Mach number is close to one.

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References

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  1. Department of Mechanical and Aerospace Engineering, University of California, Davis, CA, USA

    J. J. Chattot & M. M. Hafez

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Chattot, J.J., Hafez, M.M. (2015). Introduction to Hypersonic Flows. In: Theoretical and Applied Aerodynamics. Springer, Dordrecht. https://doi.org/10.1007/978-94-017-9825-9_12

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