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Nomogram for correcting drag and angle of attack of an airfoil model in an air stream of finite diameter
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1924 |
| Description | In experimenting with airfoil models in a wind tunnel, the magnitude of the forces acting on the model is affected by the fact that the air stream in which the model is suspended, has a restricted cross-section. In order to utilize the results for an airplane in an unlimited quantity of air, a correction must be made. The magnitude of this correction was determined by Prandtl by the application of his wing theory. |
| File Size | 519672 |
| Page Count | 8 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930086637 |
| Archival Resource Key | ark:/13960/t9g47w58h |
| Language | English |
| Publisher Date | 1924-01-01 |
| Access Restriction | Open |
| Subject Keyword | Mathematics Airfoils - Angle OF Attack - Wind Tunnel Correction Drag - Airfoils - Windtunnel Correction Nomographs - Airfoils 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 |
