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Model experiments to evaluate vortex dissipation devices proposed for installation on or near aircraft runways
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Kohl, R. E. |
| Copyright Year | 1973 |
| Description | The effectiveness of various vortex dissipation devices proposed for installation on or near aircraft runways is evaluated on basis of results of experiments conducted with a 0.03-scale model of a Boeing 747 transport aircraft in conjunction with a simulated runway. The test variables included type of vortex dissipation device, mode of operation of the powered devices, and altitude, lift coefficient and speed of the generating aircraft. A total of fifteen devices was investigated. The evaluation is based on time sequence photographs taken in the vertical and horizontal planes during each run. |
| File Size | 79810441 |
| Page Count | 189 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740009846 |
| Archival Resource Key | ark:/13960/t70w37z46 |
| Language | English |
| Publisher Date | 1973-08-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Models Photographic Recording Boeing 747 Aircraft Runways Simulation Vortex Breakdown Blast Deflectors Performance 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 |
