带受控振荡附翼的新概念旋翼气动弹性分析

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1999, Vol. 20 ›› Issue (2): 161-163.

Previous Articles Next Articles

AEROELASTIC ANALYSIS OF NEW CONCEPT ROTOR BLADE WITH CONTROLLED OSCILLATING TRAILING EDGE FLAP

Yang Weidong, Zhang Chenglin, Wang Shicun, Gu Zhongquan

Research Institute of Helicopter Technology, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016

Received:1998-05-20 Revised:1998-10-05 Online:1999-04-25 Published:1999-04-25

Abstract

Abstract:

The aeroelastic analysis of a helicopter rotor blade with the controlled oscillating trailing edge flap is presented by building an aeroelastic model of the new concept rotor blade.The aerodynamic model with unsteady terms including the effect of the trailing edge flap has been used.The sensitivity of structural parameters of the trailing edge flap on vibration reduction is also studied.Numerical results show that significant reductions of vibratory vertical shears and hub moments in the fixed frame can be obtained for a four bladed soft inplane hingeless rotor.

Key words: helicop ter, ro to r, aeroelast icity, flap, vibrat ion

CLC Number:

Yang Weidong;Zhang Chenglin;Wang Shicun;Gu Zhongquan. AEROELASTIC ANALYSIS OF NEW CONCEPT ROTOR BLADE WITH CONTROLLED OSCILLATING TRAILING EDGE FLAP[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1999, 20(2): 161-163.

[1]	CHEN Xian, CHEN Cheng, HUANG Jiangtao, CHEN Qisheng, YU Longzhou, ZHONG Shidong. Effects of belly flap on take-off and landing characteristics of a flying-wing vehicle [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(3): 125028-125028.
[2]	NIAN Peng, SONG Bifeng, XUAN Jianlin, WANG Siqi. Modeling method for propulsion system of flapping wing vehicles [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(9): 224646-224646.
[3]	PENG Liansong, ZHENG Mengzong, PAN Tianyu, SU Guanting, LI Qiushi. Effects of tandem-wing interactions on aerodynamics of hovering dragonflies [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(7): 124571-124571.
[4]	ZHANG Hongzhi, SONG Bifeng, SUN Zhongchao, WANG Liang. Driving mechanism of flapping wing aircraft: Review and prospect [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(2): 24024-024024.
[5]	LIU Jieping, MA Yuanhong, CAI Qiaoyan, REN Shaojie, WANG Suning, YANG Zimeng. Wind tunnel experiment on supersonic exhaust flow of symmetric reusable space vehicles [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(2): 624043-624043.
[6]	LIU Jing, WANG Chao, XIE Peng, ZHOU Chaoying. Development of insect-like flapping wing micro air vehicle based on PD control [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(9): 223678-223678.
[7]	ZHANG Wei, LIU Xinjie, LIU Yan, WANG Wenbo, ZHANG Boli. Flapping mechanism with elastic components: dynamic analysis and experiment [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(9): 423559-423559.
[8]	ZHOU Jinlong, DONG Linghua, YANG Weidong. Hysteresis modeling and suppression of piezoelectric actuator for helicopter trailing-edge flaps [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(4): 223384-223384.
[9]	HUANG Yong. Flight test technic for flap operation load with optical fiber sensing [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(4): 223213-223213.
[10]	MENG Min, JIANG Xian, JIA Tianjiao. A flap crank load measurement method based on virtual load calibration test [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(2): 223408-223408.
[11]	LI Kangkang, CHEN Weiwei. Variable stiffness design of flapping wings and its effects on lift and thrust [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(11): 423785-423785.
[12]	ZHANG Minghui, CHEN Zhenli, MAO Jun, WANG Gang, TAN Zhaoguang, WANG Long, ZHANG Binqian. Design of Krueger flap for civil aircraft with blended-wing-body [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(9): 623048-623048.
[13]	MA Kaichao, XU Lanling, ZHANG Jianye. Flight load design of aileron of carrier-based transport category aircraft [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(4): 622262-622262.
[14]	HAN Zhirong, ZHAO Keliang, YAN Wei. Application of Gurney flap in hybrid-wing design for icing wind tunnel [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(2): 522387-522387.
[15]	ZHANG Wei, LIU Guangze, ZHANG Boli. Energy consumption comparative analysis and research of flapping wing vehicle with elastic damping flapping mechanism [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(9): 421966-421979.

AEROELASTIC ANALYSIS OF NEW CONCEPT ROTOR BLADE WITH CONTROLLED OSCILLATING TRAILING EDGE FLAP

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments