Design and component integration of a T63-A-700 gas turbine engine test facility
A gas turbine engine test cell was developed integrating an Allison T63-A-700 helicopter engine with a superflow water brake dynamometer power absorber. Design specifications were set on all systems and subsystems necessary to operate the engine. Preliminary and detailed designs of the air, water, f...
| Main Author: | |
|---|---|
| Other Authors: | |
| Language: | en_US |
| Published: |
Monterey, California. Naval Postgraduate School
2013
|
| Online Access: | http://hdl.handle.net/10945/35129 |