Subsonic Wind Tunnel Wall Interference Correction Method Using Data Mining and Multi-Layer Perceptron

Author:

Bak Jongseo,Tai Myungsik,Park Donghun,Jeong Shinkyu

Funder

Agency for Defense Development

Publisher

Springer Science and Business Media LLC

Reference47 articles.

1. Rasuo B (2006) On status of wind tunnel wall correction. 25th ICAS CONGRESS

2. Garner HC, Rogers EW, Accum WE, Maskell EC (1966) Subsonic wind tunnel wall corrections. AGARD-AG-109, NATO

3. Labruje TE, Maarsingh RA, Smith J (1988) Evaluation of measured-boundary-condition methods for 3D subsonic wall interference. NLR-TR-88072-U, NLR

4. Rueger M, Crites R, Weirich R (1995) Comparison of conventional and emerging (‘measured variable’) wall correction techniques for tactical aircraft in subsonic wind tunnels. In 33rd Aerospace Sciences Meeting and Exhibit p 108. https://doi.org/10.2514/6.1995-108

5. Kang SH, Kwon OJ, Ahn SK (2005) Blockage correction method for separated flows over an aircraft in a closed test-section wind tunnel. J Korean Soc Aeronaut Space Sci 33:42–49. https://doi.org/10.5139/JKSAS.2005.33.8.042

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