6
Theories on Hovering Flight of Insects
79
where,
R
is reacting force of the flier.
dm
dt
is the rate of mass flow of air passing over the wings.
M f
is the mass of the flier and
g
is the acceleration due to gravity.
The rate of mass flow of air during flight is considered as a function of disc area
(Sd), effective wing breadth (Beff), the density of air ρ and wingbeat frequency of
flier (ϑh).
dm
dt α Sd Bef f ρ ϑh
2
(6.3)
The wingbeat cycle consists of an upstroke followed by a downstroke. In a flap-
ping cycle, as the downstroke of the wing is considered to be more powerful and
contributes to maximum lift than upstroke (recovery stroke), half of the value of wing-
beat frequency
ϑh
2
is included in the above equation as it is derived on an empirical
basis. The frequency arrived at the above equation agrees well with experimental
observations.
R α dm
dt
R α Sd Bef f ρ ϑh
2
(6.4)
or
R = kSd Bef f ρ ϑh
2
(6.5)
From Eqs. 6.2 and 6.5, we get
M f g = kSd Bef f ρ ϑh
2
(6.6)
where
Sd = πr2 = π L2
4
,
and L = wingspan
M f g = k π L2
4
Bef f ρ ϑh
2
Rewriting this equation, we get