| DOI | Resolve DOI: https://doi.org/10.2514/6.2020-2810 |
|---|
| Author | Search for: Davison, Craig R.1; Search for: Fuleki, Dan1; Search for: Kroff, Scott1 |
|---|
| Affiliation | - National Research Council of Canada. Aerospace
|
|---|
| Format | Text, Article |
|---|
| Conference | AIAA Aviation 2020 Forum, June 15-19, 2020, Virtual Event |
|---|
| Abstract | A heated, instrumented leading edge on the National Research Council Canada compact isokinetic probe has been developed to differentiate between liquid and solid in mixed phase icing conditions. The system was tested in an altitude wind tunnel under fully glaciated conditions and with increasing levels of melt. This paper describes the operation and presents test results. The melt ratio from the compact isokinetic probe is compared to a multi-element hot wire probe and a 1 D model for calculating evaporation, particle temperature and melt. |
|---|
| Publication date | 2020-06-08 |
|---|
| Publisher | American Institute of Aeronautics and Astronautics |
|---|
| In | |
|---|
| Language | English |
|---|
| Peer reviewed | Yes |
|---|
| Export citation | Export as RIS |
|---|
| Report a correction | Report a correction (opens in a new tab) |
|---|
| Record identifier | 8b0d6fc9-db61-4cd9-81d9-71a1814f83d3 |
|---|
| Record created | 2022-01-21 |
|---|
| Record modified | 2022-01-21 |
|---|
