摘要: Wing rock in the F-15 was examined both analytically and experimentally. Using apreviously developed model for the F-15, bifurcation analysis and continuation techniques were used to map out the periodic wing rock solutions and th... 展开
作者 | Davison, M. T. | ||
---|---|---|---|
原报告号 | ADA256613 | 总页数 | 169 |
报告类别/文献类型 | AD / NTIS科技报告 | ||
关键词 | Wings Jet fighters Architecture Computers Constants Control Feedback Feeding Flight History Mach number Maps Models Motion Parameters Predictions Rates Rock Roll Rudders Simulation Stability Test and evaluation Time Theses |