Abstract
The stability of an elastic plate and an elastic panel placed in a supersonic gas flow is studied in a nonlinear formulation. The gas velocity vector is directed at a small angle to them. The critical velocity of the flow is determined for various parameter values. The numerical results obtained are compared.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.