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Analytical investigation of rotor wake formation and geometry
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Murman, E. M. Miller, R. |
| Copyright Year | 1986 |
| Description | A number of refinements in the computer code were worked out and tested. Three codes have been written to date. One program is for an isolated wing and is being used to compare with data for the vortex wake (Weston). The second code is for an isolated wing with a streamwise vortex passing above it. This program is being used to validate the computational procedure for incorporating the vortex into the Euler equation calculations. The third program is the hovering rotor code which is the overall objective of the research. The optimization calculations for a hovering helicopter rotor have been completed. |
| File Size | 582563 |
| Page Count | 21 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19860020296 |
| Archival Resource Key | ark:/13960/t49p7xq0t |
| Language | English |
| Publisher Date | 1986-01-16 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Turbulent Wakes Wings Computational Fluid Dynamics Helicopters Vortices Rotors Proving Rotor Blades Leading Edges Computer Programs Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
