Projects funded by the NCN
Development of advanced estimation methods for blade vibration parameters and stress level in axial compressor
2011/01/D/ST8/07612
Keywords:
turbomachinery axial compressor blade vibration tip-timing Campbell diagram high cycle fatigue
Descriptors:
- ST8_1: Chemical engineering, technical chemistry, environmental engineering, sanitary engineering, engineering of chemical processes
- ST8_6: Mechatronics, fine mechanics
Panel:
ST8 - Production and processes engineering: modelling, product design, process design and control, construction methods and engineering, power units and systems
Host institution :
Instytut Techniczny Wojsk Lotniczych
woj. mazowieckie
Principal investigator (from the host institution):
Number of co-investigators in the project: 7
Call: SONATA 1 - announced on 2011-03-15
Amount awarded: 328 900 PLN
Project start date (Y-m-d): 2011-12-15
Project end date (Y-m-d): 2014-12-14
Project duration:: 36 months (the same as in the proposal)
Project status: Project settled