| Download | - View final version: The design of fluid anti-icing systems (PDF, 2.7 MiB)
|
|---|
| DOI | Resolve DOI: https://doi.org/10.4224/40003355 |
|---|
| Author | Search for: Smith, E. L.1; Search for: National Research Council of Canada. National Aeronautical Establishment |
|---|
| Affiliation | - National Research Council Canada
|
|---|
| Format | Text, Technical Report |
|---|
| Physical description | 28 p. |
|---|
| Abstract | The method employed in determining fluid requirements for anti-icing is outlined and calculated results for gas turbine engines and for a typical wing are presented. Experimental results verifying the theory are given.
The practical application of fluid anti-icing is discussed with special references to the gas turbine engine |
|---|
| Publication date | 1953-03 |
|---|
| Publisher | National Research Council of Canada |
|---|
| Series | |
|---|
| Language | English |
|---|
| Peer reviewed | No |
|---|
| Export citation | Export as RIS |
|---|
| Report a correction | Report a correction (opens in a new tab) |
|---|
| Record identifier | f64c5521-eb28-4569-9ff6-32b038394078 |
|---|
| Record created | 2023-01-30 |
|---|
| Record modified | 2024-07-02 |
|---|
