Research on Panel Flutter
Abstract
A computer program was developed which is particularly well suited for use in parametric flutter investigations where a large quantity of numerical data required. The underlying analysis used exact, linearized, three-dimensional aerodynamic theory so the program can be used to investigate the critical low supersonic regime. Finite panel arrays can be treated, and wind tunnel installations can be simulated. A limited quantity of informative numerical data is presented Most of the data pertains to the flutter of single panels with free side edges, with and without adjacent vertical side walls.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 01, 1964
- Accession Number
- ADA397048
Entities
People
- D. R. Kobett
Organizations
- MRIGlobal