RESEARCH ON THE FLUTTER OF AXIAL-TURBOMACHINE BLADING.
Abstract
Theoretical and experimental phases of a program to study flutter in turbomachinery blading are summarized. The analytical model serves mainly to describe the unstalled, linearized baseline from which the large amplitude, possibly stalled data may be compared. The effect of significant parameters on quasistatic aerodynamic moment is displayed and generalized conclusions are drawn. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 01, 1970
- Accession Number
- AD0710794
Entities
People
- Fernando Sisto
- Ron Ho Ni
Organizations
- Stevens Institute of Technology