This thesis reports on an experimental investigation into the trailing edge pressure and losses of a symmetrical isolated aerodynamic body under transonic flow conditions. Tests were made in the 4" x 4" transonic wind tunnel at the University of Liverpool. The test programme included bleed through three different base configurations and the effect on base pressure and losses. Experimental measurements included base pressures, static pressure variation over the model surface and wake total pressure traverses. Schlieren photographs were taken and samples of these are presented to indicate the nature of the flow in the wake region.
| Identifer | oai:union.ndltd.org:bl.uk/oai:ethos.bl.uk:539104 |
| Date | January 1980 |
| Creators | Edwards, S. J. |
| Publisher | University of Liverpool |
| Source Sets | Ethos UK |
| Detected Language | English |
| Type | Electronic Thesis or Dissertation |
Page generated in 0.0053 seconds