@article{oai:nagoya.repo.nii.ac.jp:00030739,
 author = {Choi, Jang-Soo and Chang, Keun-Shik and Sugiyama, Yoshiyuki},
 issue = {2},
 journal = {Memoirs of the Faculty of Engineering, Nagoya University},
 month = {Mar},
 note = {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.},
 pages = {337--350},
 title = {An application of the surface-singularity method to wing-body-tail configurations},
 volume = {40},
 year = {1989}
}