Accession Number:

ADA066464

Title:

Investigation of Blade Flutter of Axial Compressors by the Discrete- Phase Method

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH

Personal Author(s):

Report Date:

1978-05-30

Pagination or Media Count:

12.0

Abstract:

Subject Categories:

  • Test Facilities, Equipment and Methods
  • Fluid Mechanics
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE