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EXPERIMENTAL INVESTIGATION OF OSCILLATORY AERODYNAMIC FORCES, MOMENTS, AND PRESSURES ACTING ON A TAPERED WING OSCILLATING IN PITCH AT MACH NUMBERS FROM 0.40 TO 1.07

机译：在机械编号从0.40到1.07的间距上振动的锥形齿上的振荡气动力，力矩和压力的实验研究

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摘要

Oscillatory aerodynamic forces, moments, and pressures acting on a tapered wing oscillating in pitch

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作者
Clevenson, S. A.; Igoe, W. B.; Leadbetter, S. A.;
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年度 1962
页码 1-43
总页数 43
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC FORCES; MACH NUMBER; OSCILLATING FLOW; OSCILLATIONS; PITCHING MOMENTS; SPALLING; SWEPT WINGS; TAPERING; WING OSCILLATIONS; AERODYNAMIC FORCE; MOMENT; OSCILLATING WING; PITCHING MOMENT; TAPERED WING;

机译：空气动力学;马赫数;振荡流量;振荡; pITCHING mOmENTs;剥落; sWEpT WINGs;逐渐变细; WING OsCILLaTIONs;空气动力;时刻;振荡之翼; pITCHING mOmENT;锥形翼;

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2. Experimental study and modelling of unsteady aerodynamic forces and moment on flat plate in high amplitude pitch ramp motion [J] . Yu Yuelong, Amandolese Xavier, Fan Chengwei, Journal of Fluid Mechanics . 2018,第期

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3. Experimental investigation of aerodynamic performance of oscillating wings at low Re numbers [J] . Soylak Mustafa Proceedings of the Institution of Mechanical Engineers . 2016,第G10期

机译：低Re数摆动翼气动性能的实验研究。
4. Wind Tunnel Measurement of 6-Component Forces and Moments Acting on a Model of New Wing-In-Surface-Effect Craft of All-Wing Type for 8 Passengers [C] . Hiromichi Akimoto, Yasuhisa Matsuzaki, Yoshinori Ogawa, International EuroConference on High-Performance Marine Vehicles(HIPER'02); 20020914-17; Bergen(NO) . 2002

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5. Wind-Tunnel Measurements of the Aerodynamic Damping and Oscillatory Stability in Pitch of a Sphere at Mach Numbers from 0.20 to 4.63. [D] . Kilgore, Robert Ashworth. 1963

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6. A chordwise offset of the wing-pitch axis enhances rotational aerodynamic forces on insect wings: a numerical study [O] . Wouter G. van Veen, Johan L. van Leeuwen, Florian T. Muijres 2019

机译：机翼-俯仰轴的弦向偏移增强了昆虫机翼上的旋转空气动力：数值研究
7. Measurements of Lift, Pitching Moment and Center of Pressure of Delta Wing Body Combinations at Mach Number 1.88 [O] . Michio TAKEI 1962

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8. INVESTIGATION OF THE EFFECTS OF LEADING-EDGE FLAPS ON THE AERODYNAMIC CHARACTERISTICS IN PITCH AT MACH NUMBERS FROM 0.40 TO 0.93 OF A WING-FUSELAGEnCONFIGURATION WITH A 45° SWEPTB ACK WING OF ASPECT RATIO 4 [R] . Kenneth P. Spreemann, William J. Alford 1953

机译：利用45°sWEpTB确定宽高比4的机翼数量从0.40到0.93的机械臂间距对空气动力学特性的影响研究4

EXPERIMENTAL INVESTIGATION OF OSCILLATORY AERODYNAMIC FORCES, MOMENTS, AND PRESSURES ACTING ON A TAPERED WING OSCILLATING IN PITCH AT MACH NUMBERS FROM 0.40 TO 1.07

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