https://catalogue-scientifique.canada.ca/record=1827525~S6*frc
Office national d'études et de recherches aérospatiales, 1998
Thèse, mémoire et essai
De : Réseau des bibliothèques scientifiques fédérales
https://catalogue-scientifique.canada.ca/record=1827525~S6*frc
https://publications-cnrc.canada.ca/fra/voir/objet/?id=0cda0957-cb1b-4163-aabd-0d46f668f7be
https://publications-cnrc.canada.ca/fra/voir/objet/?id=cfb9a449-21aa-4c13-8e41-07bae854f4b5
The paper represents the second part of a study related to the development of an actuators control system for a morphing wing application, and describes the...
https://publications-cnrc.canada.ca/fra/voir/objet/?id=cdeddfaf-a22e-460b-86da-573c49656fc8
The paper presents the design phase of the actuators control system development for a morphing wing application. Some smart materials, like Shape Memory Alloy...
https://publications-cnrc.canada.ca/fra/voir/objet/?id=2ab3650a-db0c-4996-88e8-9ef8052aa3f5
In this paper, wind tunnel results of a real time optimization of a morphing wing in wind tunnel for delaying the transition towards the trailing edge are...
https://publications-cnrc.canada.ca/fra/voir/objet/?id=2c4c7828-10d2-465e-95be-467d03da751a
This paper presents the boundary layer transitional flow behaviour past a morphing experimental wing. The objective of the present investigation is to reduce...
https://publications-cnrc.canada.ca/fra/voir/objet/?id=e8d072dc-bff0-438c-adb5-21f9cacc651c
In this paper, wind tunnel experiment was performed for boundary layer transitioncontrol on a morphing wing. Surface pressure fluctuations weremeasured using...
https://publications-cnrc.canada.ca/fra/voir/objet/?id=66776e23-2969-4d7e-a0e2-cf80919765e4
https://publications-cnrc.canada.ca/fra/voir/objet/?id=25c809ee-3468-4529-8360-886d828cf7ca
The objective of this study was to assess the antimicrobial resistance and virulence genotypes of Enterococcus faecalis isolated from samples obtained from a...
https://publications-cnrc.canada.ca/fra/voir/objet/?id=ba68c400-7ae0-4e4c-a3ea-dc298d3c3d46
A large-scale multi-disciplinary research project, CRIAQ 7.1, was undertaken to investigate a morphing wing concept for aircraft aerodynamic performance...
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