Experimental study of flapping-wing aerodynamic coefficients and landing performance estimation

Aliabadi, Saeed Karimian; Parsa, Mohamad Reza; Moghadam, Majid

doi:10.1007/s11012-023-01644-7

Cited by 1 publication

(3 citation statements)

References 27 publications

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“…Alternative sensors utilize the same mounting methods as the ATI Nano 17, although some also opt to allow adjustable angles of attack [53,54]. Other sensors used include the ATI Mini 40 [55], ATI Gamma [56], F6D45 [57], Deltalab sensor [58], M3816BH [59], and other unspecified sensors [60].…”

Section: Multi-axis Load Cellmentioning

confidence: 99%

“…In this instance, the sensor is used in a tachometer to determine the operational frequency of the system. Some example systems that use this method are in references [30,[44][45][46]53,59].…”

Section: Hall Effect Sensormentioning

confidence: 99%

“…In general, wind tunnel testing is utilized in conjunction with other instrumentation methods. Depending on the target velocity of the flapping wing system under test, the systems are tested at various maximum speeds such as 3-5 ms −1 [24,36,47,52,54,60], 6-8 ms −1 [32,40,41,58,59] or 10 ms −1 [28,53,61]. This variety of chosen wind velocities is due to the wide variety of flapping wing fliers that exist in nature and their respective flight velocities.…”

Section: Wind Tunnelmentioning

confidence: 99%

See 2 more Smart Citations

A Bibliometric Analysis of Flapping Wing Instrumentation

Lefik,

Marian,

Chahl

2023

Aerospace

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There are flapping wing-style systems being developed by various institutions around the world. However, despite there being many systems that superficially appear robust, there is no viable flapping wing flying system at this time. We identified a gap in knowledge and capability, which is that the lack of appropriate instrumentation seems to be a major roadblock in further developing flapping wing flying systems. There is no complete solution in regards to instrumentation and sensing at the appropriate scales. This paper seeks to critically examine and classify the existing instrumentation utilized and reported in the literature and attempts to identify the path forward for flapping wing-style instrumentation.

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