Drag coefficient accuracy improvement by means of particle image velocimetry for a transonic NACA0012 airfoil

被引:11
作者
Ragni, D. [1 ]
van Oudheusden, B. W. [1 ]
Scarano, F. [1 ]
机构
[1] Delft Univ Technol, Fac Aerosp Engn, Delft, Netherlands
关键词
drag; pressure; PIV; accuracy; transonic; PIV;
D O I
10.1088/0957-0233/22/1/017003
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
A method to improve the reliability of the drag coefficient computation by means of particle image velocimetry measurements is made using experimental data acquired on a NACA0012 airfoil tested in the transonic regime, using the combination of a variable pulse separation with a new high-order Poisson spectral pressure reconstruction algorithm.
引用
收藏
页数:5
相关论文
共 12 条
[1]  
Anderson J.D., 1991, Fundamentals of Aerodynamics, V2nd
[2]  
[Anonymous], 2000, SIAM
[3]  
Baur T, 1999, 3 INT WORKSH PIV SAN
[4]  
CANUTO C.G., 2007, Spectral Methods
[5]  
GREGORY N, 1973, NPL9615 NACA0012 COM
[6]  
Karniadakis GE, 2005, Spectral/hp Element Methods for CFD
[7]  
Kline S.J., 1952, ASME Mechanical Engineering, V75, P3, DOI DOI 10.1016/J.CHAOS.2005.11.046
[8]   Surface pressure and aerodynamic loads determination of a transonic airfoil based on particle image velocimetry [J].
Ragni, D. ;
Ashok, A. ;
van Oudheusden, B. W. ;
Scarano, F. .
MEASUREMENT SCIENCE AND TECHNOLOGY, 2009, 20 (07)
[9]   Advances in iterative multigrid PIV image processing [J].
Scarano, F ;
Riethmuller, ML .
EXPERIMENTS IN FLUIDS, 2000, 29 (Suppl 1) :S51-S60
[10]   Principles and application of velocimetry-based planar pressure imaging in compressible flows with shocks [J].
van Oudheusden, B. W. .
EXPERIMENTS IN FLUIDS, 2008, 45 (04) :657-674