It is well known that seaplanes have twin floaters. Therefore, it is necessary to conduct a wind tunnel test that aims to determine the performance of twin floaters paired on a mock aircraft model. The twin floaters use the same scale as the mock aircraft, which is 1:6.3 with a length of 1555 mm and a distance between floaters of 668.8 mm or S/L of 0.43. The test plan uses a speed of 65 m s and a Reynolds number 1.5 times the model configuration with flap angle variations of 0°, 10°, 18°, 30°, and 40°. The final test results showed that tabulations and graphs of lift coefficient (C), drag coefficient (C), and pitching moment coefficient (C) with angle of attack (α) variations of -10° to 16°.

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http://www.ncbi.nlm.nih.gov/pmc/articles/PMC11539510PMC
http://dx.doi.org/10.1016/j.dib.2024.111008DOI Listing

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It is well known that seaplanes have twin floaters. Therefore, it is necessary to conduct a wind tunnel test that aims to determine the performance of twin floaters paired on a mock aircraft model. The twin floaters use the same scale as the mock aircraft, which is 1:6.

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