Geometry effects on autorotation of rectangular prisms

被引:9
作者
Greenwell, D. I. [1 ]
机构
[1] Aircraft Res Assoc Ltd, Bedford, England
关键词
Autorotation; Slung load; Rectangular prism; END-PLATES; SQUARE; WINGS; FLOW;
D O I
10.1016/j.jweia.2014.06.014
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
This paper presents an analysis of published data on the autorotation of rectangular prisms, supplemented by additional wind tunnel tests of container-like shapes typical of helicopter slung loads. Previous widely used correlations for effects of geometry on autorotation rate are shown to perform rather poorly, particularly for higher aspect ratios and thickness/chord ratios. A smooth and well-behaved 3D surface has been fitted to the data, permitting the likely autorotation rate of any rectangular prism to be determined graphically. Of particular significance to the behaviour of slung loads is a well-defined region where autorotation does not occur. Two new parameters for presenting autorotation data have been proposed. A normalised aspect ratio has been used which allows 2D and 3D data to be plotted on a single figure, and gives a more nearly linear variation of autorotation rate with aspect ratio. The geometric mean aspect ratio is a simple single parameter for the autorotation rate, which gives an approximate collapse of trends in the data. This parameter can be interpreted as a ratio between the strengths of driving vortices shed from spanwise and streamwise edges respectively, suggesting that the 3D structure of the flows driving autorotation would repay further investigation. (C) 2014 Elsevier Ltd. All rights reserved.
引用
收藏
页码:92 / 100
页数:9
相关论文
共 46 条
[1]   The debris flight equations [J].
Baker, C. J. .
JOURNAL OF WIND ENGINEERING AND INDUSTRIAL AERODYNAMICS, 2007, 95 (05) :329-353
[2]  
Bustamante A.C., 1967, P 7 AIAA AER SCI M N
[3]  
Bustamante A.C., 1969, P 7 AIAA AER SCI M N
[4]  
Cheng S., 1966, THESIS U BRIT COLUMB
[5]  
Cicolani L., 2010, TP2010216380 NASA
[6]   Flight Test and Simulation of a Cargo Container Slung Load in Forward Flight [J].
Cicolani, Luigi S. ;
Cone, Andrew ;
Theron, Johannes N. ;
Robinson, L. T. C. Dwight ;
Lusardi, Jeffery ;
Tischler, Mark B. ;
Rosen, Aviv ;
Raz, Reuben .
JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 2009, 54 (03) :0320061-03200618
[7]   Rotational aerophones [J].
Fletcher, NH ;
Tarnopolsky, AZ ;
Lai, JCS .
JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 2002, 111 (03) :1189-1196
[8]  
FOX TA, 1990, EXP FLUIDS, V9, P237
[9]   INFLUENCE OF END PLATES AND FREE ENDS ON THE SHEDDING FREQUENCY OF CIRCULAR-CYLINDERS [J].
GERICH, D ;
ECKELMANN, H .
JOURNAL OF FLUID MECHANICS, 1982, 122 (SEP) :109-121
[10]  
Glaser J.C., 1971, 71037 ISUERLAMES