Effects of platform friction damper on resonant stresses in gas turbine blades

Research output: Contribution to journal › Article › peer-review

Original language	English
Pages (from-to)	55
Number of pages	1
Journal	Hangkong Dongli Xuebao/Journal of Aerospace Power
Volume	16
Issue number	1
State	Published - Jan 2001

Cite this

@article{75d7d184f8bc46c5b0ca4cbf01b38851,

title = "Effects of platform friction damper on resonant stresses in gas turbine blades",

author = "Hao, \{Y. P.\} and Shan, \{Y. C.\} and Zhu, \{Z. G.\}",

year = "2001",

month = jan,

language = "英语",

volume = "16",

pages = "55",

journal = "Hangkong Dongli Xuebao/Journal of Aerospace Power",

issn = "1000-8055",

publisher = "BUAA Press",

number = "1",

}

TY - JOUR

T1 - Effects of platform friction damper on resonant stresses in gas turbine blades

AU - Hao, Y. P.

AU - Shan, Y. C.

AU - Zhu, Z. G.

PY - 2001/1

Y1 - 2001/1

UR - https://www.scopus.com/pages/publications/0034904661

M3 - 文章

AN - SCOPUS:0034904661

SN - 1000-8055

VL - 16

SP - 55

JO - Hangkong Dongli Xuebao/Journal of Aerospace Power

JF - Hangkong Dongli Xuebao/Journal of Aerospace Power

IS - 1

ER -