Accession Number:

ADA031536

Title:

Research on the Flutter of Axial Turbomachine Blading,

Descriptive Note:

Corporate Author:

STEVENS INST OF TECH HOBOKEN N J DEPT OF MECHANICAL ENGINEERING

Personal Author(s):

Report Date:

1976-10-01

Pagination or Media Count:

17.0

Abstract:

The unsteady response of a flat plate airfoil to large nonpotential flow disturbances is evaluated in the form of a translating rectangular grid of eddy-array. The singularity distribution principle in combination with the time-marching technique was used as the method of analysis. Author

Subject Categories:

  • Aircraft
  • Fluid Mechanics
  • Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE