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Supplementary calibration test of the tip-aerodynamics- and acoustics-test pressure transducers
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Watts, M. E. |
| Copyright Year | 1986 |
| Description | A calibration test is described that was performed to supplement the normal calibration of the 188 pressure transducers used in the Tip Aerodynamics and Acoustics Test. This calibration led to the identification of 15 transducers which had a slope change of greater than 7% from the initial calibration. The calibration procedure is described and the results presented. The effect of the slope changes on the pressure distributions are described, followed by a method to compensate for these changes. |
| File Size | 9311728 |
| Page Count | 44 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19870003397 |
| Archival Resource Key | ark:/13960/t3518wf23 |
| Language | English |
| Publisher Date | 1986-07-01 |
| Access Restriction | Open |
| Subject Keyword | Pressure Sensors Acoustic Measurement Calibrating Aerodynamic Coefficients Pressure Measurement Rotary Wing Aircraft Pressure Gradients Tips 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 |
