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Current laminar flow control experiments at nasa dryden
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Bowers, Al |
| Copyright Year | 2010 |
| Description | An experiment to demonstrate laminar flow over the swept wing of a subsonic transport is being developed. Discrete Roughness Elements are being used to maintain laminar flow over a substantial portion of a wing glove. This passive laminar flow technology has only come to be recognized as a significant player in airliner drag reduction in the last few years. NASA is implementing this experiment and is planning to demonstrate this technology at full-scale Bight cruise conditions of a small-to-medium airliner. |
| File Size | 754369 |
| Page Count | 16 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20110003577 |
| Archival Resource Key | ark:/13960/t3421zc4c |
| Language | English |
| Publisher Date | 2010-09-04 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Subsonic Speed Full Scale Tests Swept Wings Drag Reduction Laminar Flow Transport Aircraft Wing Planforms Surface Roughness Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Presentation |
