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
More Info
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Publication Year
2026
Language
English
Research Group
Aerodynamics
Pages (from-to)
104-110
Publisher
Springer Science and Business Media B.V.
Reuse Rights
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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.