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Tag Archives: sharp leading edge

Performance of a Transpiration-Cooled Sharp Leading Edge for Hypersonic Flight

1.Events, HiSST 2024, Thermal and Energy ManagementBy Beata Wierzbińska-PrusJune 3, 2024

Raghul RAVICHANDRAN, Luke DOHERTY, Matthew MCGILVRAY

DOI Number: N/A

Conference number: HiSST-2024-192

A Transpiration Cooled Wedge with adapted Permeability

HiSST 2018, Materials and Structures, Supersonic and Hypersonic Aircraft Design, Thermal and Energy Management Systems, Thermal Protection SystemsBy tverminOctober 13, 2023

Christian Dittert , Hannah Böhrk and Stefan Löhle

DOI Number XXX-YYY-ZZZ

Conference Number HiSST 2018-2280892

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