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Supersonic Aeroelastic Bifurcation of Nonlinear Truncated Conical Shells with Initial Stress

机译：具有初始应力的非线性截短锥形壳的超音速空气弹性分岔

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晨光范;
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1. Nonlinear supersonic flutter of truncated conical shells [J] . Journal of Mechanical Science and Technology . 2020,第4期

机译：截短锥形壳的非线性超音速颤动
2. A unified algorithm for fully-coupled aeroelastic stability analysis of conical shells in yawed supersonic flow to identify the effect of boundary conditions [J] . Rahmanian Mohammad, Javadi Masoud Thin-Walled Structures . 2020,第Octa期

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3. A FORMULATION OF THE PROBLEM ON AEROELASTIC VIBRATIONS OF A CONICAL SHELL WITH A SMALL OPENING ANGLE (THE CASE OF SUPERSONIC GAS FLOW INSIDE THE SHELL) [J] . I. A. Kiyko Moscow University Mechanics Bulletin . 2004,第3期

机译：具有小开角的圆锥形壳体的气动弹性振动问题的公式化（壳体内部有超音速气流的情况）
4. HOMOCLINIC ORBIT BIFURCATION OF A ROTATING TRUNCATED CONICAL SHELL [C] . Liming Dai, Changping Chen IMECE2009;ASME international mechanical engineering congress and exposition . 2010

机译：旋转截顶圆锥壳的同向轨道分叉
5. Aeroelastic analysis of circular cylindrical and truncated conical shells subjected to a supersonic flow. [D] . Sabri, Farhad. 2009

机译：圆柱和截锥形壳体在超音速作用下的气动弹性分析。
6. Nonlinear Stability Analysis of Eccentrically Stiffened Functionally Graded Truncated Conical Sandwich Shells with Porosity [O] . Duc-Kien Thai, Tran Minh Tu, Le Kha Hoa, 2018

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7. Effect of the nonlinear pre-buckling state on the bifurcation point of conical shells [O] . Jabareen Mahmood, Sheinman Izhak 2006

机译：非线性预屈曲状态对圆锥壳分叉点的影响
8. Stress and Stability Analysis of Cylindrical and Conical Shells. Volume I. An Infinitesimal-Buckling Analysis for Truncated Conical Shells Subjected to External Pressure [R] . Pittner, E. V., Morton, F. G. 1961

机译：圆柱壳和锥壳的应力和稳定性分析。第一卷。截断圆锥壳受外压影响的无穷小屈曲分析

Supersonic Aeroelastic Bifurcation of Nonlinear Truncated Conical Shells with Initial Stress

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