航空機の定常スピン領域の数値解析法 Numerical Analysis Method for the Steady Spin Regions of Aircraft
This paper introduces a numerical method to search the steady spin regions for aircraft. A minimization problem is set to calculate the steady spin regions of an aircraft, along with a proposed simple performance index. The spin characteristics are discussed using proposed control surfaces' margin criteria and their contour maps. Using the YF-16 data, a series of simulations were conducted to check the stable spin states calculated with the method, and control surfaces' effectiveness around the stable spin states. The simulations' results show that the proposed contour maps give useful handling information so as to change the steady spin states effectively.
- 日本航空宇宙学会論文集 = Journal of the Japan Society for Aeronautical and Space Sciences
日本航空宇宙学会論文集 = Journal of the Japan Society for Aeronautical and Space Sciences 55(646), 533-540, 2007-11-05