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A method of predicting flow rates required to achieve anti-icing performance with a porous leading edge ice protection system
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Albright, A. E. Kohlman, D. L. |
| Copyright Year | 1983 |
| Description | An analytical method was developed for predicting minimum flow rates required to provide anti-ice protection with a porous leading edge fluid ice protection system. The predicted flow rates compare with an average error of less than 10 percent to six experimentally determined flow rates from tests in the NASA Icing Research Tunnel on a general aviation wing section. |
| File Size | 1553618 |
| Page Count | 25 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19830024511 |
| Archival Resource Key | ark:/13960/t4vj0ch4c |
| Language | English |
| Publisher Date | 1983-08-01 |
| Access Restriction | Open |
| Subject Keyword | Air Transportation And Safety Ice Prevention Atmospheric Temperature Porous Materials Antiicing Additives Fluid Flow Flow Velocity Airfoils Glycols General Aviation Aircraft Prediction Analysis Techniques Leading Edges Freezing Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
