Generalized Formulation of Nonlinear Pitch-Yaw-Roll Coupling: Part 11-Nonlinear Coning-Rate Dependence
- 1 March 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 13 (3) , 327-332
- https://doi.org/10.2514/3.49699
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- The spacing, position and strength of vortices in the wake of slender cylindrical bodies at large incidenceJournal of Fluid Mechanics, 1971
- Recent Experience with Techniques for Prediction of Spin Characteristics of Fighter AircraftJournal of Aircraft, 1971
- Some Experiments with Vortex BreakdownJournal of the Royal Aeronautical Society, 1964