AbstractsEngineering
A temperature survey of the region aft of a cooling orifice of an air film cooled metal surface exposed to high temperature and high velocity gases
| Institution: | Naval Postgraduate School |
|---|---|
| Department: | Department of Aeronautical Engineering |
| Year: | 1951 |
| Record ID: | 1537790 |
| Full text PDF: | http://hdl.handle.net/10945/14709 |
Abstract
The object of this investigation was to determine the temperature pattern in the region downstream from a cooling air orifice of an air film cooled simulated turbine blade exposed to high velocity and high temperature gases. It was particularly desired to determine the pattern within the boundary layer of the flow over the blade since this pattern would indicate the degree of mixing and the extent to which the cool film remained on the blade surface.
