A dynamic analysis of the motion of a low-wing general aviation aircraft about its calculated equilibrium flat spin mode
- 11 August 1980
- conference paper
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Determination of the spin and recovery characteristics of a typical low-wing general aviation designPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Application of the equilibrium spin technique to a typical low-wing general aviation designPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- The influence of the static and dynamic aerodynamic characteristics on the spinning motion of aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1970