Acoustic phasing and amplification effects of single rotor helicopter blade-vortex interactions

被引：0

作者：

Sim, Ben Wel-C. ^{[1
]}

Schimtz, Fredric H. ^{[1
]}

机构：

[1] Univ of Maryland, College Park, United States

来源：

Annual Forum Proceedings - American Helicopter Society | 1999年 / 2卷

关键词：

D O I：

暂无

中图分类号：

学科分类号：

摘要：

引用

页码：1436 / 1450

共 50 条

[1] Acoustic phasing, directionality and amplification effects of helicopter blade-vortex interactions
Schmitz, FH
Sim, BWC
JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 2001, 46 (04) : 273 - 282
[2] Orthogonal blade-vortex interaction on a helicopter tail rotor
Filippone, Antonio
Afgan, Imran
AIAA JOURNAL, 2008, 46 (06) : 1476 - 1489
[3] Effects of surface blowing/suction on the aerodynamics of helicopter rotor blade-vortex interactions (BVI) - A numerical simulation
Hassan, AA
Straub, FK
Charles, BD
JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 1997, 42 (02) : 182 - 194
[4] Aerodynamics and acoustics of rotor blade-vortex interactions
Yu, Yung H., 1600, AIAA, Washington, DC, United States (32):
[5] AERODYNAMICS AND ACOUSTICS OF ROTOR BLADE-VORTEX INTERACTIONS
YU, YH
TUNG, C
GALLMAN, J
SCHULTZ, KJ
VANDERWALL, B
SPIEGEL, P
MICHEA, B
JOURNAL OF AIRCRAFT, 1995, 32 (05): : 970 - 977
[6] Influence of blade-to-blade dissimilarity on alleviation of helicopter blade-vortex interactions
Tauszig, L
Gandhi, F
MATHEMATICAL AND COMPUTER MODELLING, 2001, 33 (10-11) : 1139 - 1154
[7] MODEL OF BLADE-VORTEX INTERACTION IN AN INVISCID FLUID AND APPLICATION TO A HELICOPTER ROTOR
RAHIER, G
RECHERCHE AEROSPATIALE, 1995, (04): : 241 - 252
[8] Parallel blade-vortex interaction modelling for helicopter rotor noise control synthesis
Modini, Sara
Graziani, Giorgio
Bernardini, Giovanni
Gennaretti, Massimo
INTERNATIONAL JOURNAL OF AEROACOUSTICS, 2014, 13 (7-8) : 587 - 606
[9] Calculation of far field sound due to blade-vortex interaction on a helicopter rotor
Wagner, S
ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND MECHANIK, 2001, 81 : S151 - S154
[10] Reduction of helicopter blade-vortex interaction noise by active rotor control technology
Yu, YH
Gmelin, B
Splettstoesser, W
Philippe, JJ
Prieur, J
Brooks, TF
PROGRESS IN AEROSPACE SCIENCES, 1997, 33 (9-10) : 647 - 687

← 1 2 3 4 5 →