New concepts about 4 hole wall stress probe

ICIASF Record, International Congress on Instrumentation in Aerospace Simulation Facilities

Volumn 1997, Issue , 1997, Pages 223-227

  De Ponte, S ^a   Gasparini, L ^a   Gibertini, G ^a   Codazzi, L ^a  

^a POLITECNICO DI MILANO   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; CALIBRATION; FLOW MEASUREMENT; FLUID DYNAMICS; PERTURBATION TECHNIQUES; PROBES; WALL FLOW;

AIRFOIL SURFACE; FLOW PERTURBATION; FLUID STREAM; WALL SHEAR STRESS MEASUREMENT;

SHEAR STRESS;

EID: 0031378892     PISSN: 07302010     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Article

References (9)

1. B.L. Welsh, P.R. Ashill, "Pressure Measurement Technique in use at Aerospace Establishment", VKI LS 05, 1989.
2. P. Dexter, "Evaluation of a Skin-friction Vector Measuring Instrument for use in 3-D Turbulent Incompressible Flow", Project Report University of Southampton (UK) Dept. of Astronautics and Aeronautics, 1974.
3. S.E. De Ponte, M. Parrini, "A Hot-wire for detecting Wall Shear-stress direction", ICIASF '91 (Rockville, Maryland, USA), pp 270-276, 1991.
4. S.E. De Ponte, G. Gibertini, "Two-dimensional Airfoil Wakes: Experiments and Numerical Simulation", ICAS '94 (Anaheim, California, USA), pp 2375-2382, 1994.
5. R. Eppler, "Airfoil Design and Data", Springer-Verlag, Berlin, 1990.
6. H.P. Horton, "A Semi-empirical Theory for the Growth and Bursting of Laminar Separation Bubbles", ARC CP 1073, 1967.
7. J.L. Van Ingen, "Transition, Pressure Gradient, Suction, Separation and Stability Theory", AGARD CP 224, pp 20.1-20.15, 1977.
8. J.E. Green, D.J. Weeks, J.W.F. Brooman, "Prediction of Turbulent Boundary Layers and Wakes in Compressible Flow By a Lag-Entrainment Method", ARC R&M 3791, 1973.
9. G. Iuso, M. Onorato, "Skin Friction Measurements in 3-D Boundary Layers", ICEFM '91 (Chengdu, China), pp 700-705, 1991.