NASA NTRS · 19710041303
A nonlinear aerodynamic moment formulation and its implications for dynamic stability testing
Abstract
Nonlinear aerodynamic moment system for nonaxisymmetric bodies free flight motion analysis, taking into account interactions excluded in classical treatment
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Schiff, L. B., Tobak, M.. 1971-03-01. A nonlinear aerodynamic moment formulation and its implications for dynamic stability testing. https://ntrs.nasa.gov/citations/19710041303
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