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Rotational accelerations stabilize leading edge vortices on revolving fly wings
J Exp Biol Lentink and Dickinson 212: 2705
JEB022269 Supplementary Material
Files in this Data Supplement:
Movie 1
-
Movie 1.
Unstable LEV generated by a unidirectional translating swept fly wing at
Re
=1400 and
Ro
tip=inf. See Fig. 1A.
Movie 2
-
Movie 2.
Unstable LEV generated by a unidirectional translating unswept fly wing at
Re
=1400 and
Ro
tip=inf. See Fig. 1B.
Movie 3
-
Movie 3.
Stable LEV generated by a unidirectionally revolving fly wing at
Re
=110 and
Ro
tip=2.9. See Fig. 1C.
Movie 4
-
Movie 4.
Stable LEV generated by a reciprocating revolving fly wing at
Re
=110 and
Ro
tip=2.9. See Fig. 4A.
Movie 5
-
Movie 5.
Unstable LEV generated by a reciprocating translating fly wing at
Re
=110 and
Ro
tip=inf. See Fig. 4A.
Movie 6
-
Movie 6.
Stable LEV generated by a reciprocating revolving fly wing at
Re
=1400 and
Ro
tip=2.9. See Fig. 4A.
Movie 7
-
Movie 7.
Stable LEV exhibits spiral bursting at
Re
=1400 and
Ro
tip=2.9. See Fig. 4B.
This Article
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