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Effect of periodic changes of angle of attack on behavior of airfoils
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1922 |
| Description | This report presents the results of a series of experiments, which gave some quantitative results on the effect of periodic changes in the direction of the relative air flow against airfoils. The first series of experiments concerned how the angle of attack of the wing model was changed by causing the latter to oscillate about an axis parallel to the span and at right angles to the air flow. The second series embraced all the experiments in which the direction of the air flow itself was periodically changed. |
| File Size | 887515 |
| Page Count | 20 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930083152 |
| Archival Resource Key | ark:/13960/t78s7wz8z |
| Language | English |
| Publisher Date | 1922-01-01 |
| Access Restriction | Open |
| Subject Keyword | Airfoils - Angle OF Attack Katzmayr Effect Airfoils - Experimental 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 |
