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Experimental studies on the aerodynamic performance and dynamic response of flow direction sensing vanes
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Crossman, G. R. Barna, P. S. |
| Copyright Year | 1976 |
| Description | Systematic investigations were performed on a variety of aerodynamic surfaces to obtain their potential for possible application to wind vanes. Among the surfaces tested were: (1) single vanes consisting of flat plates of various planforms having aspect ratios between 0.5 and 5; (2) bi-vanes with aspect ratio 2.5; (3) various cone and box vanes; and (4) various cruciform configurations. The models were subjected to windtunnel tests. In addition to lift and drag force measurements, damping and frequency test were performed under a variety of flow conditions. |
| File Size | 3607331 |
| Page Count | 126 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760017144 |
| Archival Resource Key | ark:/13960/t3b03xv5n |
| Language | English |
| Publisher Date | 1976-05-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Instrumentation Dynamic Response Damping Tests Lift Drag Ratio Wind Vanes Wind Tunnel Tests Drag Measurement Aerodynamic Characteristics Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |