摘要: A wind tunnel investigation was conducted to study the low speed, high angle of attack stability characteristics of a three surface fighter concept based on the F-15 configuration. Static force data were measured over angle of att... 展开
作者 | Grafton, S. B. Croom, M. A. Nguyen, L. T. | ||
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原报告号 | N83-19757 | 总页数 | 60 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Canard configurations F-15 aircraft Forced vibration Lateral stability Longitudinal stability Wind tunnel tests Aerodynamic coefficients Airfoil profiles Angle of attack Chords (Geometry) Coupling Deflection Lift Low speed Sideslip |