Dynamic turbine blade temperature measurements
- 1 January 1994
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 10 (1), 69-78
- https://doi.org/10.2514/3.23713
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Low-cycle fatigue and creep analysis of gas turbine engine componentsJournal of Aircraft, 1975