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-Prus June 3, 2024

Raghul RAVICHANDRAN, Luke DOHERTY, Matthew MCGILVRAY

DOI Number: XXX-YYY-ZZZ

Conference number: HiSST2024-00192

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 tvermin October 13, 2023

Christian Dittert , Hannah Böhrk and Stefan Löhle

DOI Number XXX-YYY-ZZZ

Conference Number HiSST 2018-2280892