DOI: 10.31274/etd-180810-331
|View full text |Cite
|
Sign up to set email alerts
|

An experimental study of the vortex structures in the wake of a piezoelectric flapping plate for Nano Air Vehicle applications

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...

Citation Types

0
1
0

Publication Types

Select...
1

Relationship

0
1

Authors

Journals

citations
Cited by 1 publication
(1 citation statement)
references
References 2 publications
(16 reference statements)
0
1
0
Order By: Relevance
“…Wind Tunnel Calibration for Undergraduate Wind TunnelFlow velocities at different wind tunnel frequencies were calculated with the help of data gathered from Clemons[50]. The average flow velocities at the test section of the wind tunnel were obtained through PIV measurements at different motor frequencies.…”
mentioning
confidence: 99%
“…Wind Tunnel Calibration for Undergraduate Wind TunnelFlow velocities at different wind tunnel frequencies were calculated with the help of data gathered from Clemons[50]. The average flow velocities at the test section of the wind tunnel were obtained through PIV measurements at different motor frequencies.…”
mentioning
confidence: 99%