COMPUTATION OF TRANSONIC FLOW ABOUT HELICOPTER ROTOR BLADES

被引：2

作者：

ARIELI, R

TAUBER, ME

SAUNDERS, DA

CAUGHEY, DA

机构：

[1] NASA, AMES RES CTR, MOFFETT FIELD, CA 94035 USA

[2] INFORMAT GEN CORP, PALO ALTO, CA USA

[3] CORNELL UNIV, ITHACA, NY 14853 USA

来源：

关键词：

CENTRIFUGAL FORCES - COMPUTER CODES - CORIOLIS FORCES - HELICOPTER ROTOR BLADES - ROT22 FLOW CODE;

D O I：

10.2514/3.9338

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：722 / 727

页数：6

共 50 条

[21] Aerodynamic analysis of potential use of flow control devices on helicopter rotor blades
Tejero, F.
Doerffer, P.
Szulc, O.
XXI FLUID MECHANICS CONFERENCE, 2014, 530
[22] Deformation Analysis of Composite Rotor Blades for a Helicopter
Hou, Weiguo
Zhang, Weifang
Wang, Xiaoliang
Xing, Jun
JOURNAL OF AIRCRAFT, 2012, 49 (06): : 2018 - 2022
[23] Control of dynamic stall of helicopter rotor blades
WANG Rong
XIA PinQi
Science China(Technological Sciences) , 2013, (01) : 171 - 180
[24] Control of dynamic stall of helicopter rotor blades
Wang Rong
Xia PinQi
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2013, 56 (01) : 171 - 180
[25] EQUIVALENT G/E OF HELICOPTER ROTOR BLADES
ROSEN, A
AIAA JOURNAL, 1983, 21 (03) : 478 - 479
[26] Control of dynamic stall of helicopter rotor blades
Rong Wang
PinQi Xia
Science China Technological Sciences, 2013, 56 : 171 - 180
[27] THE DISTURBED FLAPPING MOTION OF HELICOPTER ROTOR BLADES
PARKUS, H
JOURNAL OF THE AERONAUTICAL SCIENCES, 1948, 15 (02): : 103 - 106
[28] BOUNDARY LAYER CONTROL ON HELICOPTER ROTOR BLADES
DEBONO, AN
POLLARD, MG
AIRCRAFT ENGINEERING, 1967, 39 (09): : 42 - &
[29] Preventing delamination of Robinson helicopter rotor blades
不详
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2008, 80 (02): : 228 - 228
[30] A helicopter with adaptive rotor blades for collective control
Roglin, RL
Hanagud, SV
SMART MATERIALS & STRUCTURES, 1996, 5 (01): : 76 - 88