VIBRATION AND FLUTTER OF THIN PRESSURIZED SHELLS IN SUPERSONIC FLOW.
Abstract
This report concerns the vibration and flutter of a thin pressurized shell. It consists of the following three parts: Free vibration in vacuo; Vibration in supersonic flow; and Supersonic flutter. Both structural and aerodynamical boundary conditions are taken into consideration. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1969
- Accession Number
- AD0682139
Entities
People
- Ta Li
Organizations
- General Dynamics