Loading...
Please wait, while we are loading the content...
Similar Documents
High-speed-propeller wind-tunnel aeroacoustic results
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Dittmar, J. H. Jeracki, R. J. |
| Copyright Year | 1980 |
| Description | Some aerodynamic concepts are presented together with an explanation of how these concepts are applied to advanced propeller design. The unique features of this propulsion system are addressed with emphasis on the design concepts being considered for the high speed turboprop. More particular emphasis is given to the blade sweep, long blade chords, and the large number of blades. |
| File Size | 733158 |
| Page Count | 14 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800013857 |
| Archival Resource Key | ark:/13960/t5r83528q |
| Language | English |
| Publisher Date | 1980-03-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Performance Tests Propellers Aerodynamic Configurations Noise Reduction Wind Tunnel Tests Performance Prediction Airfoils Propeller Efficiency Aeroacoustics Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
