Loading...
Please wait, while we are loading the content...
Similar Documents
Turbine blade tip durability analysis
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Spamer, G. T. Laflen, J. H. McKnight, R. L. |
| Copyright Year | 1981 |
| Description | An air-cooled turbine blade from an aircraft gas turbine engine chosen for its history of cracking was subjected to advanced analytical and life-prediction techniques. The utility of advanced structural analysis techniques and advanced life-prediction techniques in the life assessment of hot section components are verified. Three dimensional heat transfer and stress analyses were applied to the turbine blade mission cycle and the results were input into advanced life-prediction theories. Shortcut analytical techniques were developed. The proposed life-prediction theories are evaluated. |
| File Size | 5859363 |
| Page Count | 124 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810018554 |
| Archival Resource Key | ark:/13960/t96738n8c |
| Language | English |
| Publisher Date | 1981-02-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Blade Tips Component Reliability Turbine Blades Life Durability High Temperature Environments Prediction Analysis Techniques Structural Analysis Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |