Improvement of noise filtering and image registration methods for the Pressure Sensitive Paint experiments

Author:

Fujimatsu N.,Tamura Y.,Fujii K.

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Condensed Matter Physics

Reference13 articles.

1. Bell, J. H. and McLachlan, B. G., Image Registration for Luminescence Paint Sensors, AIAA Paper 93-0178, 31st Aerospace Sciences Meeting & Exhibit, (1993).

2. Egami, Y., Iijima, Y., Amao, Y., Asai, K., Fuji, A., Teduka, N. and Kameda, M., Quantitative Visualization of the Leading-edge Vortices on a Delta Wing by Using Pressure-sensitive Paint, J. of Visualization, 4-2 (2004), 139–150.

3. Burt, P. J. and Andelson, E. H., The Laplacian pyramid as a compact image code, IEEE Trans. Commun., 31-4 (1983), 532–540.

4. Erickson, G. E., Wind Tunnel Investigation of the Interaction and Breakdown Characteristics of Slender-Wing Vortices at Subsonic, Transonic and Supersonic Speeds, NASA-TP3116, (1991).

5. Koutsavdis, E. K., Blaisdell, G. A., Lyrintzis, A. S., A Numerical Investigation of Two Dimensional Jets using Spatial Filtering, 5th AIAA/CEAS Aeroacoustics Conference, AIAA-Paper 99-3706, 37th Aerospace Sciences Meeting & Exhibit, (1999).

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