Kanda A. Sting supporting system with controllable roll mode / A. Kanda, T. Ueda, 1997. - 22 p. - Текст : непосредственный.
Technical report / Nat. aerospace lab. TR-1451 : Yawing mode flutter of non-planar wing / A.Kanda, 2002. - 13 p. - Текст : непосредственный.
Technical report / Nat. aerospace lab. TR-1452 : Correction of flutter boundary of non-planar wing using measured local Mach number / A.Kanda, 2002. - 23 p. - Текст : непосредственный.
Kanda A. Anti-symmetric mode flutter of winged reentry space vehicle / A.Kanda,T.Ueda, 1997. - 24 p. - Текст : непосредственный.
Kanda A. Flutter of winged vehivles coupling with elastic pitching mode caused by the booster / A.Kanda,T.Ueda, 2001. - 18 p. - Текст : непосредственный.
Kanda A. Effects of rolling elasticity on flutter characteristics at launching configuration of re-entry space vehicle / A.Kanda,T.Ueda, 1999. - 22 p. - Текст : непосредственный.
Kanda A. Confirmation tests of ALFLEX vibration characteristics / A.Kanda,T.Sotozaki,T.Ueda, 1998. - 16 p. - Текст : непосредственный.