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Nasa,faa,onera swept-wing icing and aerodynamics: summary of research and current status
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Broeren, Andy |
| Copyright Year | 2015 |
| Description | NASA, FAA, ONERA, and other partner organizations have embarked on a significant, collaborative research effort to address the technical challenges associated with icing on large scale, three-dimensional swept wings. These are extremely complex phenomena important to the design, certification and safe operation of small and large transport aircraft. There is increasing demand to balance trade-offs in aircraft efficiency, cost and noise that tend to compete directly with allowable performance degradations over an increasing range of icing conditions. Computational fluid dynamics codes have reached a level of maturity that they are being proposed by manufacturers for use in certification of aircraft for flight in icing. However, sufficient high-quality data to evaluate their performance on iced swept wings are not currently available in the public domain and significant knowledge gaps remain.|||||||||||||||| |
| File Size | 1646451 |
| Page Count | 27 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20150019655 |
| Archival Resource Key | ark:/13960/t4zh1n71m |
| Language | English |
| Publisher Date | 2015-06-22 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Icing Ice Formation Aerodynamics Performance Tests Swept Wings Scale Models Transport Aircraft Wind Tunnel Models Computerized Simulation Three Dimensional Models Data Bases Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Presentation |
