2021
DOI: 10.1109/jsen.2020.2991785
|View full text |Cite
|
Sign up to set email alerts
|

MEMS High Temperature Gradient Sensor for Skin-Friction Measurements in Highly Turbulent Flows

Abstract: HAL is a multi-disciplinary open access archive for the deposit and dissemination of scientific research documents, whether they are published or not. The documents may come from teaching and research institutions in France or abroad, or from public or private research centers. L'archive ouverte pluridisciplinaire HAL, est destinée au dépôt et à la diffusion de documents scientifiques de niveau recherche, publiés ou non, émanant des établissements d'enseignement et de recherche français ou étrangers, des labor… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1

Citation Types

0
1
0

Year Published

2021
2021
2024
2024

Publication Types

Select...
4
1

Relationship

0
5

Authors

Journals

citations
Cited by 6 publications
(1 citation statement)
references
References 24 publications
0
1
0
Order By: Relevance
“…Developed as a compromise between hot-films and hotwires and with the objective of real flight application, the high temperature gradient micro-sensors designed at IEMN is composed of wall suspended wires, mechanically supported by periodic perpendicular micro-bridges ( [11], [12]). The sensors were successfully tested in various configurations: in low [13] and high-speed wind tunnels [14] and on models [15]. In this paper, we present the utilization of such micro-sensors for real flight experiments realized on a microlight aircraft.…”
Section: Introductionmentioning
confidence: 99%
“…Developed as a compromise between hot-films and hotwires and with the objective of real flight application, the high temperature gradient micro-sensors designed at IEMN is composed of wall suspended wires, mechanically supported by periodic perpendicular micro-bridges ( [11], [12]). The sensors were successfully tested in various configurations: in low [13] and high-speed wind tunnels [14] and on models [15]. In this paper, we present the utilization of such micro-sensors for real flight experiments realized on a microlight aircraft.…”
Section: Introductionmentioning
confidence: 99%