Improved aerothermodynamic measurements of the T63-A-700 gas turbine engine
Approved for public release, distribution unlimited--Cover. === This thesis contains an analysis of the failure of the instrumentation ring for measuring the combustor exit temperature and total pressure in the T63-A-700 gas turbine engine. An improved ring design has been constructed and installed....
| Main Author: | |
|---|---|
| Other Authors: | |
| Published: |
Monterey, California. Naval Postgraduate School
2012
|
| Online Access: | http://hdl.handle.net/10945/10045 |