Accession Number:
AD0742458
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):
Report Date:
1972-05-01
Pagination or Media Count:
41.0
Abstract:
Theoretical and experimental phases of a program to study flutter in turbomachinery blading are summarized. A general analytical method for predicting the aerodynamic characteristics of partly stalled airfoil is introduced and agrees with experimental results. The effect of location of rotation axis on quasistatic aerodynamic moment is displayed and generalized conclusions are drawn. Author
Descriptors:
Subject Categories:
- Non-electrical Energy Conversion
- Fluid Mechanics