ENGINEERING COLLECTION (SELECTED ARTICLES).
Abstract
The problem on flutter is discussed for a circular cylindrical shell of open profile, moving in a gas with supersonic speed. It is assumed that the shell on its limiting longitudinal and transverse margins has hinged immobile fastenings in the planes of these margins. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 27, 1963
- Accession Number
- AD0449227
Entities
Organizations
- National Air and Space Intelligence Center