Simultaneous multi-design point approach to gas turbine on-design cycle analysis for aircraft engines
Gas turbine engines for aircraft applications are required to meet multiple performance and sizing requirements, subject to constraints established by the best available technology level. The performance requirements and limiting values of constraints that are considered by the cycle analyst conduct...
| Main Author: | |
|---|---|
| Published: |
Georgia Institute of Technology
2009
|
| Subjects: | |
| Online Access: | http://hdl.handle.net/1853/28169 |