Accession Number:

AD0687671

Title:

A NOTE ON AXISYMMETRICAL FLUTTER OF CIRCULAR CYLINDRICAL SHELLS OF FINITE LENGTH,

Descriptive Note:

Corporate Author:

DEUTSCHE VERSUCHSANSTALT FUER LUFT- UND RAUMFAHRT E V FREIBURG-IM-BREISGAU (WEST GERMANY)

Personal Author(s):

Report Date:

1968-01-16

Pagination or Media Count:

4.0

Abstract:

Krumhaar investigated the stability of axisymmetrical oscillations of a circular cylindrical shell of finite length in a supersonic airstream parallel to the cylinder axis he studied the corresponding eigenvalue problem, calculated the eigenvalues and derived the exact flutter boundaries. In the present note, the mode shapes of axisymmetrical oscillations in a neighbourhood of these flutter boundaries are investigated. Author

Subject Categories:

  • Structural Engineering and Building Technology
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE