@inproceedings{Mukhopadhyay1995InteractiveFA, title={Interactive Flutter Analysis and Parametric Study for Conceptual Wing Design}, author={Vivek Mukhopadhyay}, year={1995} }

- Published 1995

An interactive computer program was developed for wing flutter analysis in the conceptual design stage. The objective was to estimate the flutter instability boundary of a flexible cantilever wing, when well defined structural and aerodynamic data are not available, and then study the effect of change in Mach number, dynamic pressure, torsional frequency, sweep, mass ratio, aspect ratio, taper ratio, center of gravity, and pitch inertia, to guide the development of the concept. The software was… CONTINUE READING