THE APPLICATION OF AERO GAS TURBINE ENGINE MONITORING SYSTEMS TO MILITARY AIRCRAFT
- Author(s):
- BURGESS, C A R ( GRANFIELD INSTITUTE OF TECHNOLOGY )
- Publication title:
- NASA Technical Reports
- Pub. Year:
- 1990
- No.:
- N91-19096
- Paper no.:
- N91-19096
- Page(from):
- 1
- Page(to):
- 187
- Pages:
- 187
- Pub. info.:
- National Aeronautics and Space Adminstration
- Language:
- English
- Type:
- Technical Paper
Similar Items:
National Aeronautics and Space Administration |
7
Technical Paper
The New Potential for Joint UK/US Studies in Sensor Technology for HCF Studies in Gas Turbine Aero-Engines.
American Institute of Aeronautics and Astronautics |
"Society of Automotive Engineering, Inc." |
American Institute of Aeronautics and Astronautics |
"Society of Automotive Engineering, Inc." |
9
Technical Paper
Computational & Experimental Investigations of Jet Noise Reduction Concepts for Low-Bypass Ratio Military Gas Turbine Engines.
American Society of Mechanical Engineers |
4
Technical Paper
The Experimental Validation of Tip-Timing Techniques for Condition Monitoring of HCF in Gas Turbine Aero-Engines.
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
11
Technical Paper
Detailed chemical modelling predictions of emissions from a reheated gas turbine engine with application to future supersonic aircraft
The American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
The American Society of Mechanical Engineers |