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Modified Barrowman Method With Applications to the OPDAMS (Optical Deep Attack Missile Systems) and PDAMS (Precision Deep Attack Missile Systems) Vehicles

机译:改进的Barrowman方法及其在OpDams(光学深度攻击导弹系统)和pDams(精确深度攻击导弹系统)车辆中的应用

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The Barrowman Method is an accurate, low-cost algorithm for the calculation of aerodynamic parameters for rockets. The method has been modified to allow the use of airfoiled wings and fins with control surfaces and to include the effects of downwash from the wings on the fins. It has been shown that interdigitation of the wings and fins significantly reduces the downwash. The Modified Barrowman Method has been applied to PDAMS and compared to wind tunnel results. An aerodynamic model of the OPDAMS vehicle was generated. (Author).

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