摘要: The feasibility of using forebody tangential blowing to control the roll-yaw motion of a wind tunnel model is experimentally demonstrated. An unsteady model of the aerodynamics is developed based on the fundamental physics of the ... 展开
作者 | Pedreiro, N. Rock, S. M. Celik, Z. Z. Roberts, L. | ||
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原报告号 | N19960045735 | 总页数 | 54 |
主办者 | National Aeronautics and Space Administration, Washington, DC. | ||
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Aircraft control Blowing Feedback control Flight control Flow visualization Roll Wind tunnel models Wind tunnel tests Yawing moments Aerodynamic loads Angle of attack Body-wing configurations Control systems design Degrees of freedom Delta wings Dynamic loads Equations of motion Forebodies Mathematical models Static loads |