Research on the Flutter of Axial-Turbomachine Blading.
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)
Document Details
- Document Type
- Technical Report
- Publication Date
- May 01, 1972
- Accession Number
- AD0742458
Entities
People
- Fernando Sisto
- Ron Ho Ni
Organizations
- Stevens Institute of Technology