@techreport{oai:jaxa.repo.nii.ac.jp:00043757,
 author = {遠藤, 浩 and 林, 良生 and 海老沼, 幸成 and 中谷, 輝臣 and ENDO, Hiroshi and HAYASHI, Yoshio and EBINUMA, Yukinari and NAKAYA, Teruomi},
 month = {Mar},
 note = {The low-subsonic rotary dynamic derivatives of a conventional type of airplane, FA-200 modified, were measured by means of the forced-oscillation apparatus in the NAL 6m low- speed wind-tunnel. The results were compared with the theoretical values calculated by the standard estimation formulae worked out by various authors.  It is shown that the calculated values are in fairly good agreement with the measured ones, except when the separation of air-flow is supplsed to occur on the wings in course of the pitching oscillation. The accuracy of measurement of Cnr was rather low, presumably becacuse the vertical tail moved, crossing the unsteady wake behind the fuselage, in yawing oscillation., 資料番号: NALTM0173000, レポート番号: NAL TM-173},
 title = {FA-200改機の動安定微係数},
 year = {1970}
}