Experimental models

E. Zussman, Alexander Yarin, D. Weihs

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

Modeling of thrip wings for flapping unmanned aerial vehicle was carried out. Thrips wings was modeled using wing span 0.81 mm, average chord (rod length) 0.3 mm rod diameter 1.5 micron, and distance to diameter ratio was 10:1. The total normalized drag exerted on ellipsoids on the edge and in the center of a row moving along the normal direction. The results show that the length scale for Reynold number was rod diameter, NOT body size.

Original languageEnglish
Title of host publicationAUVSI's Unmanned Systems North America 2004 - Proceedings
Pages823-830
Number of pages8
Publication statusPublished - 2004 Dec 1
EventAUVSI's Unmanned Systems North America 2004 - Proceedings - Anaheim, CA, United States
Duration: 2004 Aug 32004 Aug 5

Other

OtherAUVSI's Unmanned Systems North America 2004 - Proceedings
CountryUnited States
CityAnaheim, CA
Period04/8/304/8/5

Fingerprint

Unmanned aerial vehicles (UAV)
Drag
Reynolds number

ASJC Scopus subject areas

  • Engineering(all)

Cite this

Zussman, E., Yarin, A., & Weihs, D. (2004). Experimental models. In AUVSI's Unmanned Systems North America 2004 - Proceedings (pp. 823-830)

Experimental models. / Zussman, E.; Yarin, Alexander; Weihs, D.

AUVSI's Unmanned Systems North America 2004 - Proceedings. 2004. p. 823-830.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Zussman, E, Yarin, A & Weihs, D 2004, Experimental models. in AUVSI's Unmanned Systems North America 2004 - Proceedings. pp. 823-830, AUVSI's Unmanned Systems North America 2004 - Proceedings, Anaheim, CA, United States, 04/8/3.
Zussman E, Yarin A, Weihs D. Experimental models. In AUVSI's Unmanned Systems North America 2004 - Proceedings. 2004. p. 823-830
Zussman, E. ; Yarin, Alexander ; Weihs, D. / Experimental models. AUVSI's Unmanned Systems North America 2004 - Proceedings. 2004. pp. 823-830
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