EXPERIMENTAL DETERMINATION OF VARIATION OF HYDROFOIL FLUTTER SPEED WITH MASS RATIO.
Abstract
A description of the design and fabrication of a family of four hydrofoil flutter models is given. These models had identical geometric and elastic properties, differing only in mass ratio. The heaviest was a direct half-scale model of an earlier flutter model. A flutter point was approached to within an estimated 1/2 knot with the heavier model, and it was near the value predicted by scaling considerations. No flutter points were measured with the three remaining models, however, as the torsional divergence speed was lower than flutter speeds for them. This was rather unexpected, as the elastic axis was at the quarter-chord--usually considered to be far enough forward to ensure a high divergence speed. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 01, 1970
- Accession Number
- AD0708061
Entities
People
- Guido E. Ransleben Jr.
Organizations
- Southwest Research Institute