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机译:UW-5006跨音速自然层流翼的设计与测试
Piaggio Aero Industries, 80078 Naples, Italy;
rnCentro Italiano Ricerche Aerospaziali, 81043 Capua, Italy Applied Aerodynamics Laboratory;
rnCentro Italiano Ricerche Aerospaziali, 81043 Capua, Italy Applied Aerodynamics Laboratory;
rnCentro Italiano Ricerche Aerospaziali, 81043 Capua, Italy Transonic Testing Group;
b: wing span; C_D: drag coefficient; C_(Dw): wave drag coefficient; C_L: lift coefficient; C_p: pressure coefficient; et al;
机译:UW-5006跨音速自然层流翼的设计与测试
机译:低雷诺数延长自然层流翼型的空气动力学设计优化
机译:高雷诺数条件下的超音速自然层流翼设计概念
机译:通过基于代理的全局优化设计跨音速自然层流(NLF)机翼的空气动力学设计
机译:重新审视空气动力学设计修改,缩短跨越跨翼翼和克鲁姆兰的临界压力系数规则
机译:变形翼尖驱动系统的基于模糊逻辑的控制:设计数值模拟和风洞实验测试
机译:自然层流翼型和翼型设计的伴随法和自动过渡预测