Accession Number:

AD0760354

Title:

Research on the Flutter of Axial-Turbomachine Blading.

Descriptive Note:

Technical rept.,

Corporate Author:

STEVENS INST OF TECH HOBOKEN N J DEPT OF MECHANICAL ENGINEERING

Personal Author(s):

• Sisto,Fernando
• Perumal,P. V. K.

Report Date:

1973-05-02

Pagination or Media Count:

39.0

Abstract:

An analytical method for predicting the perturbed aerodynamic reactions of a harmonically oscillating flat plate airfoil with time dependent point of separation is presented. It is shown that this method in conjunction with an empirical knowledge of the time history of the separation point can predict stall flutter. Numerical results are presented and compared with existing theoretical and experimental results. Author

Descriptors:

• (*TURBINE BLADES
• STALLING)
• FLUTTER
• OSCILLATION
• CASCADE STRUCTURES
• FLOW SEPARATION
• VIBRATION
• AEROELASTICITY
• NUMERICAL ANALYSIS

Subject Categories:

• Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE