Accession Number : AD0449227
Title : ENGINEERING COLLECTION (SELECTED ARTICLES).
Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Report Date : 27 Dec 1963
Pagination or Media Count : 1
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)
Descriptors : FLUTTER , SHELLS(STRUCTURAL FORMS) , SUPERSONIC FLOW , EQUATIONS , PANELS , STABILITY
Distribution Statement : APPROVED FOR PUBLIC RELEASE