Flared Folding Wingtips - TU Delft

This collection contains the results of the work carried out at the TU Delft regarding the flared folding wingtips (FFWT) concept. The FFWT is a concept where the wingtip of an airplane can be folded when the airplane is on the ground, deployed during flight to increase aerodynamic efficiency, and released in-flight as a means of load alleviation.<br>In this collection, we present the numerical simulations and experimental data related to the FFWT studies conducted at the TU Delft. The naming convention for the datasets presented in this collection is "XYYY - NAME (Month Year)(Data underlying the publication: NOP)", where:X: Type of study (E-Experiment, M - Numerical Model)YYY: Order number within the type of study. For example, E001_ for the first experiment, E002_ for the second experiment, etc.NAME: name of the respective studyMonth Year: in the case of the experiment, the date when the experiment was conducted. For models, the date when the model is archived.NOP: Name of publication, if exists.

本数据集收录了代尔夫特理工大学（TU Delft）针对flare折叠翼尖（flared folding wingtips，FFWT）概念开展研究的成果。FFWT概念是指飞机翼尖可在地面状态下折叠，飞行时展开以提升气动效率，并能在飞行过程中释放以实现载荷减缓。<br>本数据集中呈现了代尔夫特理工大学FFWT研究相关的数值模拟与实验数据。数据集的命名规则为“XYYY - NAME（Month Year）（Data underlying the publication: NOP）”，其中：X代表研究类型（E-实验，M-数值模型）；YYY为该类型研究内的序号（例如，E001表示首个实验，E002表示第二个实验等）；NAME为对应研究的名称；Month Year对于实验而言指研究开展日期，对于模型而言指模型归档日期；NOP为出版物名称（若存在）。