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Results: 1-7 |
Results: 7
Asymptotic analysis of aircraft wing model in subsonic air flow
Authors: Shubov, MA
Citation: Ma. Shubov, Asymptotic analysis of aircraft wing model in subsonic air flow, IMA J APP M, 66(4), 2001, pp. 319-356
Asymptotics of eigenfrequencies and eigenmodes of non-homogeneous inextensible filament with an end load
Authors: Shubov, MA Belinskiy, BP Martin, CF
Citation: Ma. Shubov et al., Asymptotics of eigenfrequencies and eigenmodes of non-homogeneous inextensible filament with an end load, MATH METH A, 24(15), 2001, pp. 1139-1167
Asymptotic representations for root vectors of nonselfadjoint operators and pencils generated by an aircraft wing model in subsonic air flow
Authors: Shubov, MA
Citation: Ma. Shubov, Asymptotic representations for root vectors of nonselfadjoint operators and pencils generated by an aircraft wing model in subsonic air flow, J MATH ANAL, 260(2), 2001, pp. 341-366
Asymptotics of aeroelastic modes and basis property of mode shapes for aircraft wing model
Authors: Shubov, MA
Citation: Ma. Shubov, Asymptotics of aeroelastic modes and basis property of mode shapes for aircraft wing model, J FRANKL I, 338(2-3), 2001, pp. 171-185
Riesz basis property of root vectors of non-self-adjoint operators generated by aircraft wing model in subsonic airflow
Authors: Shubov, MA
Citation: Ma. Shubov, Riesz basis property of root vectors of non-self-adjoint operators generated by aircraft wing model in subsonic airflow, MATH METH A, 23(18), 2000, pp. 1585-1615
Spectral operators generated by Timoshenko beam model
Authors: Shubov, MA
Citation: Ma. Shubov, Spectral operators generated by Timoshenko beam model, SYST CONTR, 38(4-5), 1999, pp. 249-258
Boundary and distributed controllability of the damped wave equation: Reduction of control time
Authors: Shubov, MA Martin, CF
Citation: Ma. Shubov et Cf. Martin, Boundary and distributed controllability of the damped wave equation: Reduction of control time, J MATH ANAL, 240(1), 1999, pp. 16-36
Risultati: 1-7 |