NASA NTRS · 19800000087
Aircraft equilibrium spin characteristics
Abstract
Program provides analytic solutions to nonlinear equations of motion describing spin conditions. Stability characteristics also are determined. Program can be used to study effects of aerodynamic and inertial parameters on spin and could be modified to compute equilibrium conditions for steady maneuvers. Program is written in FORTRAN IV for batch execution on CYBER 173.
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Adams, W. M., Jr.. 1980-08-01. Aircraft equilibrium spin characteristics. https://ntrs.nasa.gov/citations/19800000087
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