Force measurements on a circular cylinder in a Cryogenic Ludwieg-Tube using piezoelectric transducers

被引:7
作者
Schewe, Guenter [1 ]
Steinhoff, Christian [1 ]
机构
[1] DLR, Inst Aeroelast, Gottingen, Germany
关键词
D O I
10.1007/s00348-007-0250-1
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Force and pressure measurements were performed in a high Reynolds number facility, i.e. the Cryogenic Ludwieg-Tube (KRG). The balance based on multicomponent piezoelectric force transducers was applied totally in the cryogenic environment. The behaviour of the balance was tested ranging from ambient down to cryogenic conditions. As test cases, the flow around a circular cylinder was investigated at a sub- and supercritical Mach number. The highest possible Reynolds number in most nearly incompressible flow (Re = 5.8 x 10(6)) was achieved at the temperature of T = -150 degrees C, the highest pressure possible, p(0) = 10 bar, and the lowest attainable Mach number of Ma = 0.28. The results show that, in spite of the pulse operating mode of the tunnel, the steady and unsteady processes can be measured very well by means of a piezoelectric balance.
引用
收藏
页码:489 / 494
页数:6
相关论文
共 13 条
[1]  
Gautschi G., 2006, PIEZOELECTRIC SENSOR
[2]  
LUDWIEG H, 1955, 3 ZFW, P206
[3]  
ROSEMANN H, 1997, CRYOGENIC LUDWIEG TU
[4]  
SCHEINMAN SJ, 1985, MINER ELECTROL METAB, V11, P85
[6]   Nonlinear effects in transonic flutter with emphasis on manifestations of limit cycle oscillations [J].
Schewe, G ;
Mai, H ;
Dietz, G .
JOURNAL OF FLUIDS AND STRUCTURES, 2003, 18 (01) :3-22
[7]   NONLINEAR FLOW-INDUCED RESONANCES OF AN H-SHAPED SECTION [J].
SCHEWE, G .
JOURNAL OF FLUIDS AND STRUCTURES, 1989, 3 (04) :327-348
[8]   Reynolds-number effects in flow around more-or-less bluff bodies [J].
Schewe, G .
JOURNAL OF WIND ENGINEERING AND INDUSTRIAL AERODYNAMICS, 2001, 89 (14-15) :1267-1289
[9]  
SCHEWE G, 1982, SENSORS SYSTEMS 82, V2, P12
[10]  
SCHEWE G, 1991, INT FOR AER STRUCT D