NASA NTRS · 19850014068
Two degree-of-freedom flutter solution for a personal computer
Abstract
A computer programmed flutter solution has been written in the BASIC language for a personal computer. The program is for two degree-of-freedom bending torsion flutter applications and utilizes two dimensional Theodorsen aerodynamics. The aerodynamics were modified to include approximations for Mach number (compressibility) effects and aspect ratio (finite span) effects. Input options, user instructions, program listing, and a test case application are included.
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Turnock, D. L.. 1985-02-01. Two degree-of-freedom flutter solution for a personal computer. https://ntrs.nasa.gov/citations/19850014068
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