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Calibration of averaging total pressure flight wake rake and natural-laminar-flow airfoil drag certification
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Snyder, M. H. Irani, E. |
| Copyright Year | 1988 |
| Description | An averaging total pressure wake rake used by the Cessna Aircraft Company in flight tests of a modified 210 airplane with a laminar flow wing was calibrated in wind tunnel tests against a five-tube pressure probe. The model generating the wake was a full-scale model of the Cessna airplane wing. Indications of drag trends were the same for both instruments. |
| File Size | 920290 |
| Page Count | 27 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19880016059 |
| Archival Resource Key | ark:/13960/t8wb02p1s |
| Language | English |
| Publisher Date | 1988-02-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Pressure Sensors Aerodynamic Drag Laminar Flow Airfoils Calibrating Wakes Cessna 210 Aircraft Wind Tunnel Models Pressure Measurement Rakes Certification Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |