Pressure correction schemes and the use of the Wiener deconvolution method in pneumatic systems with short tubes

Experiments in Fluids

Volumn 53, Issue 3, 2012, Pages 829-837

  Semaan, Richard ^a   Scholz, Peter ^a  

^a TECHNICAL UNIVERSITY OF BRAUNSCHWEIG   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AXIAL VELOCITY; CORRECTION SCHEMES; DECONVOLUTION METHOD; FLOW EXPERIMENTS; INVERSE TRANSFER; PARTICLE IMAGES; PNEUMATIC SYSTEM; PRESSURE CORRECTION; PRESSURE DISTORTIONS; PRESSURE TUBES; REYNOLDS STRESS DISTRIBUTION; SHORT TUBE; WIENER FILTERS;

DYNAMIC RESPONSE; EXPERIMENTS; PNEUMATIC CONTROL; PNEUMATIC EQUIPMENT; REYNOLDS NUMBER; SHEAR FLOW; STRESS CONCENTRATION;

TUBES (COMPONENTS);

EID: 84868616854     PISSN: 07234864     EISSN: None     Source Type: Journal    
DOI: 10.1007/s00348-012-1332-2     Document Type: Article

References (19)

1. Anderson RC, Englund DR (1971) Liquid-filled pressure measuring systems; a method for determining frequency response. Tech. Rep. TN D-6603, NASA
2. Berg H, Tijdeman H (1965) Theoretical and experimental results for the dynamic response of pressure measuring systems. Tech. Rep. NLR-TR-F238, National Aerospace Laboratory, Amsterdam
3. Chen J, Haynes BS, Fletcher DF (2000) Cobra probe measurements of mean velocities, Reynolds stresses and higher-order velocity correlations in pipe flow. Exp Therm Fluid Sci 21:206-217 (Pubitemid 30354991)
4. Everett KN, Gerner AA, Durston DA (1983) Seven-hole cone probes for high angle flow measurement: Theory and calibration. AIAA J 21:992-998 (Pubitemid 13573894)
5. Hooper JD, Musgrove AR (1997) Reynolds stress, mean velocity, and dynamic static pressure measurement by a four-hole pressure probe. Exp Therm Fluid Sci 15:375-383
6. Hougen JO, Martin OR, Walsh RA (1963) Dynamics of pneumatic transmission lines. Control Eng 10(3):114-117
7. Iberall AS (1950) Attenuation of oscillatory pressures in instrument lines. J Res Natl Bureau Stand, vol 45, pp 85-108
8. Irwin HPAH, Cooper KR, Girard R (1979) Correction of distortion effects caused by tubing systems in measurements of fluctuating pressures. J Ind Aerodyn 5:93-107 (Pubitemid 10427737)
9. Kobayashi H, Leger T, Wolff JM (1998) Experimental and theoretical frequency response of pressure transducers for high speed turbomachiner. In:34th AIAA/ASME/SAE/ASEE joint propulsion meeting, AIAA Paper 98-3745
10. Lavoie P, Avallone G, De Gregorio F, Romano GP, Antonia RA (2007) Spatial resolution of PIV for the measurement of turbulence. Exp Fluids 43:39-51 (Pubitemid 47152154)
11. Matsunaga S, Ishibashi H, Nishi M (1980) Measurement of instantaneous pressure and velocity in nonsteady three-dimensional water flow by means of a combined five-hole probe. Trans ASME J Fluid Eng 102:196-202 (Pubitemid 11449000)
12. Naughton JW, Cattafesta LN, Settles GG (1993) Miniature, fast-response five-hole conical probe for supersonic flow field measurements. AIAA J 31(3):453-458
13. Pao YH (1965) Structure of turbulent velocity and scalar fields at large wavenumbers. Phys Fluids 8(6):1063-1975
14. Schneider GM, Hooper JD, Musgrove AR, Nathan GJ, Luxton RE (1997) Velocity and Reynolds stresses in a precessing jet flow. Exp Fluids 22:489-495 (Pubitemid 126586158)
15. Strike JA, Hind MD, Saini MS, Naughton JW, Wilson MD, Whitmore SA (2010) Unsteady surface pressure reconstruction on an oscillating airfoil using the wiener deconvolution method. In:27th AIAA Aerodynamic measurement technology and ground testing conference, Chicago, Illinois, AIAA 2010-4799
16. Treaster AL, Yocum AM (1979) The calibration and application of five-hole probes. In: ISA Transactions, vol 18, pp 23-34
17. Whitmore SA, Wilson MD (2011) Wiener deconvolution for reconstruction of pneumatically-attenuated pressure signals. AIAA J 49(5):890-897
18. Wyngaard JC (1968) Measurement of small-scale turbulence with hot wires. J Sci Instr 1(2):1105-1108
19. Zilliac GG (1993) Modelling, calibration, and error analysis of seven-hole pressure probes. Exp Fluids 14:104-120