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An experimental study of dynamic stall on advanced airfoil sections. volume 3; hot-wire and hot film measurements
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | McAlister, K. W. Lambert, O. Pucci, S. L. Carr, L. W. McCroskey, W. J. |
| Copyright Year | 1982 |
| Description | Detailed unsteady boundary layer measurements are presented for eight airfoils oscillated in pitch through the dynamic stall regime. The present report (the third of three volumes) describes the techniques developed for analysis and evaluation of the hot film and hot wire signals, offers some interpretation of the results, and tabulates all the cases in which flow reversal has been recorded. |
| File Size | 2301704 |
| Page Count | 74 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19830009234 |
| Archival Resource Key | ark:/13960/t5q864p9p |
| Language | English |
| Publisher Date | 1982-12-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Hot-wire Anemometers Pressure Distribution Oscillations Data Processing Airfoils Unsteady Flow Signal Analysis Aerodynamic Stalling Heat Transfer Boundary Layers Hot-film Anemometers Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |