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An application of wake survey rakes to the experimental determination of thrust for a propeller driven aircraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Tsai, H. J. Miley, S. J. Hall, K. R. |
| Copyright Year | 1981 |
| Description | The lack of slipstream static pressure distribution seriously affected the results but recommendations for removing the deficiency are discussed. The wake survey rake is shown to be a valuable tool in aircraft flight testing. Flow characteristics in the wake of the propeller were examined. |
| File Size | 2761602 |
| Page Count | 78 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810007471 |
| Archival Resource Key | ark:/13960/t6g20t355 |
| Language | English |
| Publisher Date | 1981-02-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Flight Tests Aerodynamic Drag Propeller Slipstreams Aircraft Wakes Flow Characteristics Cavitation Flow General Aviation Aircraft Ground Effect Aerodynamics Drag Measurement Thrust Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
