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Fluid/Structural/Thermal/Dynamics Interaction (FSTDI) in Hypersonic Flow

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A Modern Course in Aeroelasticity

Part of the book series: Solid Mechanics and Its Applications ((SMIA,volume 264))

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Abstract

Hypersonic flight is a major technical challenge and substantial efforts are currently underway to provide the understanding and technology required to design and operate effectively and safely a hypersonic aircraft for commercial or military purposes. Leyva [1] has recently described the essence of this challenge. The present chapter provides a summary of the past, present and proposed work for fluid/structural/thermal dynamics interaction.

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Authors and Affiliations

  1. Mechanical Engineering and Materials Science Duke University, Durham, NC, USA

    Earl H. Dowell

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  1. Earl H. Dowell
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Correspondence to Earl H. Dowell .

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  1. Department of Mechanical Engineering and Materials Science, Duke University, Durham, NC, USA

    Earl H. Dowell

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Dowell, E.H. (2022). Fluid/Structural/Thermal/Dynamics Interaction (FSTDI) in Hypersonic Flow. In: Dowell, E.H. (eds) A Modern Course in Aeroelasticity. Solid Mechanics and Its Applications, vol 264. Springer, Cham. https://doi.org/10.1007/978-3-030-74236-2_16

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  • DOI: https://doi.org/10.1007/978-3-030-74236-2_16

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  • Publisher Name: Springer, Cham

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  • Online ISBN: 978-3-030-74236-2

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