2024-03-28T12:50:10Z
https://nagoya.repo.nii.ac.jp/oai
oai:nagoya.repo.nii.ac.jp:00030739
2023-01-16T05:13:22Z
320:2524:2544:2551
An application of the surface-singularity method to wing-body-tail configurations
Choi, Jang-Soo
101971
Chang, Keun-Shik
101972
Sugiyama, Yoshiyuki
101973
1989-03-31
A computer code based on the 1st order panel method is presented for solving inviscid incompressible flow fields about 3-D airplane-like bodies. A sample problem chosen for a test is solved and a comparison with other computational results shows good agreement. To increase the accuracy of the method, especially for a thin wing, the number of doublet panels on the camber surface of a wing is multiplied in the chordwise direction by a factor, which enhances the accuracy to some extent.
departmental bulletin paper
Faculty of Engineering, Nagoya University
1989-03-31
Memoirs of the Faculty of Engineering, Nagoya University
2
40
337
350
0027-7657
eng