Open AccessThe analysis and testing of blade platform friction dampers used in the high pressure fuel turbopump [HPFTP] of the space shuttle main engine [SSME]
Author(s) -
Robert J. Dominic
Publication year - 1983
Publication title -
the journal of the acoustical society of america
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.619
H-Index - 187
eISSN - 1520-8524
pISSN - 0001-4966
DOI - 10.1121/1.2020627
Subject(s) - damper , vibration , nozzle , structural engineering , turbine blade , turbine , mechanical engineering , engineering , acoustics , physics
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