A unified algorithm for fully-coupled aeroelastic stability analysis of conical shells in yawed supersonic flow to identify the effect of boundary conditions-Reference-Cited by-同舟云学术

A unified algorithm for fully-coupled aeroelastic stability analysis of conical shells in yawed supersonic flow to identify the effect of boundary conditions

Published:2020-10 Issue: Volume:155 Page:106910
ISSN:0263-8231
Container-title:Thin-Walled Structures
language:en
Short-container-title:Thin-Walled Structures

Author:

Rahmanian Mohammad,Javadi Masoud

Publisher

Elsevier BV

Subject

Mechanical Engineering,Building and Construction,Civil and Structural Engineering

Reference48 articles.

1. Finite-element solution of the supersonic flutter of conical shells;Bismarck-Nasr;AIAA J.,1979

2. Optimum cone angles in aeroelastic flutter;Sunder;Comput. Struct.,1983

3. Finite element analysis of 3-ply laminated conical shell for flutter;Sunder;Int. J. Numer. Methods Eng.,1983

4. Finite-element application to rocket nozzle aeroelasticity;Mason;J. Propul. Power,1986

5. Dynamics of a conical shell containing supersonic gas flow;Aleksandrov;J. Appl. Math. Mech.,1994

Cited by 13 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. The aeroelastic stability characteristics of a ring-stiffened conical three-layered sandwich shell with an FG auxetic honeycomb core utilizing zig-zag shell theory;Aerospace Science and Technology;2024-12

2. Equivalent single layer and layerwise models for flutter and buckling analysis of supersonic variable stiffness laminated composite plates;Thin-Walled Structures;2023-10

3. Aerothermoelastic Analysis of Porous 2D Curved Panels;Journal of Vibration Engineering & Technologies;2023-09-05

4. Aerothermoelastic Analysis of Conical Shell in Supersonic Flow;Applied Sciences;2023-04-12

5. Effect of variable thickness on the aeroelastic stability boundaries of truncated conical shells;Waves in Random and Complex Media;2022-12-16