Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Pierre Schrooyen"'
Publikováno v:
Aerotecnica Missili & Spazio. 100:207-224
This work deals with the analysis of the cork P50, an ablative thermal protection material (TPM) used for the heat shield of the qarman Re-entry CubeSat. Developed for the European Space Agency (ESA) at the von Karman Institute (VKI) for Fluid Dynami
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1eb746bde19745097ffb6eb0400e3040
https://doi.org/10.1007/s42496-021-00084-4
https://doi.org/10.1007/s42496-021-00084-4
Publikováno v:
AIAA AVIATION 2021 FORUM.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::904ed89ec33969669ef8038217923a27
https://doi.org/10.2514/6.2021-2742
https://doi.org/10.2514/6.2021-2742
Publikováno v:
AIAA AVIATION 2021 FORUM.
We study the ablation and transient thermal response of a quartz sample in air plasma. The experiment is carried out in the Plasmatron facility of the von Karman Institute for Fluid Dynamics. The aero-thermodynamic environment reproducing the atmosph
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7939e51bb6ab820f997683291cd2c9d5
https://doi.org/10.2514/6.2021-3137
https://doi.org/10.2514/6.2021-3137
Publikováno v:
ESAFORM 2021.
Microscopic defects may occur during powder-bed fusion processes which originate from molten pool instabilities. To investigate this issue, a numerical model focusing on the interaction between laser and powder, melt pool formation and thermodynamics
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c768306ed081ba8bdf967dd3d45d383a
https://doi.org/10.25518/esaform21.2441
https://doi.org/10.25518/esaform21.2441
Publikováno v:
International Journal of Thermal Sciences. 134:639-652
Ablative materials are extensively used in aerospace applications to protect the integrity of the spacecraft during atmospheric entry. Both thermal and mechanical stresses have to be withstood in the severe operating conditions typical of space missi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3a2f205ba713db393c66a1f7b336e0d5
https://doi.org/10.1016/j.ijthermalsci.2018.08.014
https://doi.org/10.1016/j.ijthermalsci.2018.08.014
Publikováno v:
International Journal of Heat and Mass Transfer. 103:108-124
The interaction between a chemically reactive boundary layer and an ablative material is one of the most challenging phenomena to model when predicting the heat load during atmospheric entries of spacecraft. The gas-material interactions are usually
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e1d06940c4459a9f88f87a7de5095def
https://doi.org/10.1016/j.ijheatmasstransfer.2016.07.022
https://doi.org/10.1016/j.ijheatmasstransfer.2016.07.022
Publikováno v:
47th AIAA Thermophysics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::39a05d24dd79c50a7bf88a7393f5496a
https://doi.org/10.2514/6.2017-3684
https://doi.org/10.2514/6.2017-3684
Publikováno v:
Scopus-Elsevier
The interaction between the mechanisms of ablation and boundary layer transition is one of the phenomena that leads to difficulties in heat-flux prediction during atmospheric entries. The objective of this work is to develop a computational tool base
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1c1d120f4ccaa2526bc5518e0eeec249
https://doi.org/10.2514/6.2013-2457
https://doi.org/10.2514/6.2013-2457
Publikováno v:
Fluid Mechanics and its Applications ISBN: 1402040482
Nonlinear traveling wave solutions to the Navier—Stokes equations in the plane Poiseuille geometry (Waleffe, F. (2003), Phys. Fluids 15, 1517–1534) come into existence through a saddle-node bifurcation at a Reynolds number of 977, very close to t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cd06d1e23f55d3ede557626ba5a13ff1
https://doi.org/10.1007/1-4020-4049-0_16
https://doi.org/10.1007/1-4020-4049-0_16
