Analytical model for ACSR approach to vibration reduction in a helicopter rotor-flexible fuselage system

被引：0

|

作者：

Univ of California, Los Angeles, United States ^{[1
]}

机构：

来源：

Aeronaut J | / 1009卷 / 399-408期

关键词：

D O I：

暂无

中图分类号：

学科分类号：

摘要：

引用

收藏

相关论文

共 50 条

[21] Overview of rotor blades optimum design for helicopter vibration reduction
Xiang, J.W.
Guo, J.X.
Zhang, X.G.
Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2001, 27 (01): : 32 - 35
[22] EXPERIMENTAL AND ANALYTICAL STUDIES OF A MODEL HELICOPTER ROTOR IN HOVER
CARADONNA, FX
TUNG, C
VERTICA, 1981, 5 (02): : 149 - 161
[23] Helicopter Fuselage Model Drag Reduction by Active Flow Control Systems
De Gregorio, Fabrizio
JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 2019, 64 (02)
[24] Aeroelastic analysis of rotor/fuselage/landing gears coupled system for helicopter during rotor starting process on the ground
Yang, W.-D. (ywdae@nuaa.edu.cn), 1600, Nanjing University of Aeronautics an Astronautics (26):
[25] ANALYTICAL APPROACH TO THE INDUCED FLOW OF A HELICOPTER ROTOR IN VERTICAL DESCENT
WANG, SC
JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 1990, 35 (01) : 92 - 98
[26] Experiments of vibration reduction effect of particle damping on helicopter rotor blade
Duan, Yong
Chen, Qian
Lin, Sha
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2009, 30 (11): : 2113 - 2118
[27] OPTIMAL PLACEMENT OF TUNING MASSES FOR VIBRATION REDUCTION IN HELICOPTER ROTOR BLADES
PRITCHARD, JI
ADELMAN, HM
AIAA JOURNAL, 1990, 28 (02) : 309 - 315
[28] Optimal placement of tuning masses for vibration reduction in helicopter rotor blades
Pritchard, Jocelyn I., 1600,
[29] Vibration Analyses Using Rotor-Elastic Fuselage Coupled Models for a Medium-Class Utility Helicopter
Bang, Shin-Won
Kim, Dong-Gyue
Park, Jae-Sang
Kim, Do-Hyung
Kang, Woo-Ram
JOURNAL OF THE KOREAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2024, 52 (02) : 157 - 166
[30] Empirical algorithm of aerodynamic interaction effects of rotor wake on fuselage for helicopter based on model experiments
2000, Zhongguo Kongqi Dongli Yanjiu yu Fazhan Zhongxin, China (14):

← 1 2 3 4 5 →