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Full-scale investigation of the aerodynamic characteristics of a sailwing of aspect ratio 5.9

机译：对纵横比5.9的帆翼的空气动力学特性进行全面调查

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Aerodynamic characteristics of full scale model sailwing with aspect ratio 5.9

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作者
Fink, M. P.;
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年度 1969
页码 1-32
总页数 32
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC CONFIGURATIONS; ASPECT RATIO; WIND TUNNEL STABILITY TESTS; AERODYNAMIC COEFFICIENTS; GRAPHS (CHARTS); LIFT DRAG RATIO; SCALE MODELS; WING LOADING; WING ROOTS;

机译：空气动力学配置;宽高比;风洞稳定性试验;空气动力学系数;图表（图表）;升降比;尺度模型; WING LOaDING; WING ROOTs;

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2. Experimental study of the aerodynamic characteristics of a low-aspect-ratio flat plate array in a configuration of interest for a tidal energy converter [J] . F. Fedoul, L. Parras, C. del Pino, Journal of Fluids and Structures . 2014,第Null期

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3. Component and Vehicle Aerodynamic Characteristics of a Low Aspect Ratio Winged Aerospace Vehicle Configuration [J] . S Chaudhuri, V Shanmugam, J Umakant Journal of the Institution of Engineers (Inida). Aerospace Engineering Division Board . 2006,第Nov期

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4. Investigation into Aerodynamic Characteristics and Flow Structures of Rectangular Flat-plate Wings of Very Small Aspect Ratios at All Angle of Attack [C] . Yusuke NISHIZAKI, Akira URITA, Shuji TANAKA 日本機械学会年次大会 . 2003

机译：在所有攻角中对极小纵横比的矩形平板翼的空气动力学特性和流动结构
5. AN INVESTIGATION OF THE THEORETICAL AND EXPERIMENTAL AERODYNAMIC CHARACTERISTICS OF A LOW-CORRECTION WIND TUNNEL WALL CONFIGURATION FOR AIRFOIL TESTING. [D] . MALEK, AHMED FOUAD HASSAN. 1983

机译：用于翼型测试的低校正风洞墙构型的理论和实验气动特性研究。
6. Full-scale experimental investigation of deposition and corrosion of pre-protector and 3rd superheater in a waste incineration plant [O] . Wenchao Ma, Terrence Wenga, Nan Zhang, -1

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7. Theoretical Investigation of Unsteady Aerodynamic Characteristics of Sailwing Airfoil Taking Account of Damping Forces. [O] . Kiyoshi Nishimoto, Keiji Takahashi 1994

机译：探测力考虑锚翼翼型不稳定空气动力学特性的理论研究。
8. Full-Scale Investigation of the Aerodynamic Characteristics of a Sailwing of Aspect Ratio 5.9 [R] . Fink, M. P. 1969

机译：对纵横比5.9的航行气动特性的全面研究

Full-scale investigation of the aerodynamic characteristics of a sailwing of aspect ratio 5.9

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