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Wake profile measurements of fixed and oscillating flaps
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Owen, F. K. |
| Copyright Year | 1984 |
| Description | Although the potential of laser velocimetry for the non-intrusive measurement of complex shear flows has long been recognized, there have been few applications in other small, closely controlled laboratory situations. Measurements in large scale, high speed wind tunnels are still a complex task. To support a study of periodic flows produced by an oscillating edge flap in the Ames eleven foot wind tunnel, this study was done. The potential for laser velocimeter measurements in large scale production facilities are evaluated. The results with hot wire flow field measurements are compared. |
| File Size | 1342850 |
| Page Count | 40 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840026357 |
| Archival Resource Key | ark:/13960/t6838nb0b |
| Language | English |
| Publisher Date | 1984-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Laser Doppler Velocimeters Wind Tunnels Data Acquisition Shear Flow Hot-wire Flowmeters Pressure Distribution Transonic Speed Unsteady Flow Velocity Distribution Data Reduction Wings Wind Tunnel Tests Aircraft Wakes Trailing Edge Flaps Velocity Measurement Data Sampling Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
