Zobrazeno 1 - 1
of 1
pro vyhledávání: '"Ch. L. Ganesh"'
Publikováno v:
Defence Science Journal. 36:9-26
This paper is concerned with the vibration characteristics of a gas-turbine blade-disk assembly and a third stage of compressor blade-disk assembly of an orpheus aircraft engine. The assembly is analyzed by considering each component individually and
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a0c877bc8e4c3938b8b7cd61295afe07
https://doi.org/10.14429/dsj.36.5956
https://doi.org/10.14429/dsj.36.5956
