Zobrazeno 1 - 8
of 8
pro vyhledávání: '"Cis G. De Maesschalck"'
Publikováno v:
Entropy
Volume 21
Issue 6
Entropy, Vol 21, Iss 6, p 604 (2019)
Volume 21
Issue 6
Entropy, Vol 21, Iss 6, p 604 (2019)
Rapid aerodynamic design and optimization is essential for the development of future turbomachinery. The objective of this work is to demonstrate a methodology from 1D mean-line-design to a full 3D aerodynamic optimization of the turbine stage using
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::45fc792a18d482a760ef7f93d314d254
Publikováno v:
Volume 5B: Heat Transfer.
The leakage flows within the gap between the tips of unshrouded rotor blades and the stationary casing of high-speed turbines are the source of significant aerodynamic losses and thermal stresses. In the pursuit for higher component performance and r
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d112ae9c0f8129ae95267e8603cb3105
https://doi.org/10.1115/gt2018-76567
https://doi.org/10.1115/gt2018-76567
Publikováno v:
Volume 5B: Heat Transfer.
Blade tip design and tip leakage flows are crucial aspects for the development of modern aero-engines. The inevitable clearance between stationary and rotating parts in turbine stages generates high-enthalpy unsteady leakage flows that strongly reduc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::896cb858b42f71186510166500ae9c79
https://doi.org/10.1115/gt2018-76564
https://doi.org/10.1115/gt2018-76564
Publikováno v:
53rd AIAA/SAE/ASEE Joint Propulsion Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bc0a420d6b82a452247a6372572356d0
https://doi.org/10.2514/6.2017-4816
https://doi.org/10.2514/6.2017-4816
Autor:
Jake Harry, Sam Otto, Matthew Klein, Andres Porro Carvalhar, Paht Juangphanich, Shawn Olsavsky, Timothee L. Pourpoint, Brian McGuire, Cis G. De Maesschalck, Robert A. White, Edmond Abdou
Publikováno v:
55th AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d4d80e58d2eaee16d155c1a7abb26a26
https://doi.org/10.2514/6.2017-0300
https://doi.org/10.2514/6.2017-0300
Publikováno v:
55th AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a5e5047790b46eb7bd2f9b8aaf102e15
https://doi.org/10.2514/6.2017-0110
https://doi.org/10.2514/6.2017-0110
Autor:
Sergio Lavagnoli, David Gonzalez Cuadrado, Valeria Andreoli, Guillermo Paniagua, Cis G. De Maesschalck
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6c3dec76b8164e618365554f96d993a6
https://doi.org/10.2514/6.2016-0910
https://doi.org/10.2514/6.2016-0910
Publikováno v:
Volume 5B: Heat Transfer.
Turbine rotor tips and casings are vulnerable to mechanical failures due to the extreme thermal loads they undergo during engine service. In addition to the heat flux variations during the engine transient operation, periodic unsteadiness occurs at e
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d11f3e93426b114701e39eca61468371
https://doi.org/10.1115/gt2014-25291
https://doi.org/10.1115/gt2014-25291