DNS of Mach 8 Transitional Flow over Low-Temperature Ablator Compression Ramp

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DNS of Mach 8 Transitional Flow over Low-Temperature Ablator Compression Ramp

Book Chapter (2026)

Author(s)

A. O. Başkaya (TU Delft - Aerospace Engineering)

S. Hickel (TU Delft - Aerospace Engineering)

Research Group

Aerodynamics

DOI related publication

https://doi.org/10.1007/978-3-032-19268-4_16 Final published version

To reference this document use

https://resolver.tudelft.nl/uuid:c4f55d7c-c72c-4abc-be05-b77ec0d38539

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Publication Year

2026

Language

English

Research Group

Aerodynamics

Pages (from-to)

104-110

Publisher

Springer Nature

Downloads counter

8

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Abstract

Designing heat shields that protect spacecraft during entry into a planetary atmosphere has been, and remains to be, one of the most critical challenges faced by aerothermodynamicists.

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