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机译:Nonslender Delta Wing在大振幅上的动态提升特性
Beihang Univ BUAA Key Lab Aeroacoust Minist Ind & Informat Technol Lu Shijia Lab Beijing 100191 Peoples R China|Beihang Univ BUAA Inst Fluid Mech Key Lab Fluid Mech Minist Educ Beijing 100191 Peoples R China;
Beihang Univ BUAA Key Lab Aeroacoust Minist Ind & Informat Technol Lu Shijia Lab Beijing 100191 Peoples R China|Beihang Univ BUAA Ningbo Inst Technol Aircraft & Prop Lab Ningbo 315800 Peoples R China|Delft Univ Technol Fac Aerosp Engn Flight Performance & Prop Sect FPP NL-2629 HS Delft Netherlands;
Beihang Univ BUAA Key Lab Aeroacoust Minist Ind & Informat Technol Lu Shijia Lab Beijing 100191 Peoples R China|Beihang Univ BUAA Inst Fluid Mech Key Lab Fluid Mech Minist Educ Beijing 100191 Peoples R China;
Beihang Univ BUAA Key Lab Aeroacoust Minist Ind & Informat Technol Lu Shijia Lab Beijing 100191 Peoples R China|Beihang Univ BUAA Inst Fluid Mech Key Lab Fluid Mech Minist Educ Beijing 100191 Peoples R China;
Delft Univ Technol Fac Aerosp Engn Flight Performance & Prop Sect FPP NL-2629 HS Delft Netherlands;
Hamburg Univ Appl Sci Dept Automot & Aeronaut Engn Hamburg Germany;
Nonslender delta wing; Pitching oscillations; Unsteady aerodynamics; Hysteresis;
机译:柔性不修长三角翼的提升能力
机译:格尼襟翼对裁剪后的细长三角翼升力的影响
机译:自由旋转的细长和不细长三角翼的涡流动力学
机译:俯仰运动中非柔性三角翼的气动特性。
机译:非人的人和三角洲翅膀的空气动力学
机译:飞行方式对固定升力面对禽翼空气动力学特性的影响
机译:非细长三角翼的非定常空气动力学
机译:机械编号4.04的两个三角翼的气动特性以及机械臂数从1.62到6.9的三角翼的最小和最小拖曳数据的相关性