On the aeroelastic characteristics of the forward swept wing optimized by Aeroelastic Tailoring / J. Nakamichi, H. Ejiri, T. Kikuchi, M. Minegishi, 1993. - 12 p. - Текст : непосредственный.
Vibration testing of a 1/5 scale model of H-II launch vehicle / M.Minegishi,M.Sano,K.Komatsu и др., 1990. - 154 p. - Текст : непосредственный.
Technical report / Nat.aerospace lab. TR-1461 : Vertical drop test a YS-11 fuselage section / M.Minegishi,K.Iwanski,I.Kumakura;Minegishi M., Iwanski K., Kumakura I. et al., 2003. - 59 p. - Текст : непосредственный.
Ground vibration test of the NAL Dornier 228-200 flight research airplane / Y.Ando,M.Minegishi,M.Hashidate и др., 1995. - 20 p. - Текст : непосредственный.
Estimation of critical values and vibration characteristics on supersonic delta wings. Pt. 2 : Locally-stationary time series analysis of nonstationary random responses / M.Minegishi,Y.Ando,Y.Matsuzaki и др., 1992. - 19 p. - Текст : непосредственный.