NONLINEAR EFFECTS IN HELICOPTER ROTOR FORWARD FLIGHT FORCED RESPONSE

被引：0

|

作者：

MATHEW, MB

LOEWY, RG

机构：

来源：

VERTICA | 1990年 / 14卷 / 01期

关键词：

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

收藏

页码：1 / 18

页数：18

相关论文

共 50 条

[1] CHAOTIC STALL RESPONSE OF HELICOPTER ROTOR IN FORWARD FLIGHT
TANG, DM
DOWELL, EH
JOURNAL OF FLUIDS AND STRUCTURES, 1992, 6 (03) : 311 - 335
[2] WAKE STRUCTURE OF A HELICOPTER ROTOR IN FORWARD FLIGHT
BRIASSULIS, G
ANDREOPOULOS, J
JOURNAL OF AIRCRAFT, 1993, 30 (04): : 459 - 466
[3] Wake structure of a helicopter rotor in forward flight
Briassulis, G.
Andreopoulos, J.
Journal of Aircraft, 1993, 30 (04): : 459 - 466
[4] Computation of helicopter rotor acoustics in forward flight
Strawn, RC
Biswas, R
JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 1995, 40 (03) : 66 - 72
[5] Aeroelastic analysis of a helicopter rotor in forward flight
Buchtala, B
Hierholz, KH
Wagner, S
HIGH PERFORMANCE COMPUTING IN SCIENCE AND ENGINEERING '99, 2000, : 327 - 330
[6] ON THE DAMPING IN PITCH OF A HELICOPTER ROTOR IN FORWARD FLIGHT
GEBHARD, DF
GOLAND, L
JOURNAL OF THE AERONAUTICAL SCIENCES, 1956, 23 (11): : 1051 - 1052
[7] FLUTTER OF A HELICOPTER ROTOR BLADE IN FORWARD FLIGHT
STAMMERS, CW
AERONAUTICAL QUARTERLY, 1970, 21 : 18 - &
[8] Investigation of Rotor Noise Shielding Effects by the Helicopter Fuselage in Forward Flight
Yin, Jianping
JOURNAL OF AIRCRAFT, 2019, 56 (04): : 1677 - 1688
[9] GENERIC ICING EFFECTS ON FORWARD FLIGHT PERFORMANCE OF A MODEL HELICOPTER ROTOR
TINETTI, AF
KORKAN, KD
VERTICA, 1989, 13 (01): : 63 - 85
[10] STABILITY OF A FLEXIBLE HELICOPTER ROTOR BLADE IN FORWARD FLIGHT
SHULMAN, Y
JOURNAL OF THE AERONAUTICAL SCIENCES, 1956, 23 (07): : 663 - &

← 1 2 3 4 5 →