Collocation Flutter Analysis Study II (COFA II). Volume 3. Structural Analysis Program - FLUENC-100C Component Mode Synthesis Program - COMSYN and Modal Flutter Analysis Program
Abstract
This study covers the development of a set of computer programs to perform flutter analysis. These programs supplement those of collocation flutter Analysis-Study I Contract No. 00019-68-C-0274. This study is presented in three volumes. Volume I contains a subsonic strip theory unsteady aerodynamics program and a supersonic pison theory unsteady aerodynamics program. Volume II contains unsteady aerodynamic generalized force programs for subsonic, transonic, and supersonic flight regimes. Volume III contains the structural analysis programs, FLUENC-100C and COMSYN, and the modal flutter analysis program.
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 01, 1970
- Accession Number
- AD0872191
Entities
Organizations
- Hughes Aircraft Company