PowerToFroMechChem {afpt} | R Documentation |
Convert between mechanical and chemical power
Description
Functions convert between mechanical and chemical power
Usage
mech2chem(power.mech,bird,...)
chem2mech(power.chem,bird,...)
Arguments
power.mech |
Numerical value for mechanical power |
power.chem |
Numerical value for chemical power |
bird |
object describing the relevant morphological parameters of the bird (or bat); this object should be created using the |
... |
optional arguments (none yet) |
Details
Chemical power is computed as
P_\mathrm{chem} = R(\frac{P_\mathrm{mech}}{\eta} + \mathrm{BMR})
as described in Pennycuick 2008. Here R
is the respiration factor, \eta
is the muscle conversion efficiency and \mathrm{BMR}
the basal metabolic rate, see Bird
.
Mechanical power is simply calculated inversely:
P_\mathrm{mech} = \eta(\frac{P_\mathrm{chem}}{R} - \mathrm{BMR})
Value
Numerical value of either chemical power (mech2chem()
) or mechanical power (chem2mech()
).
Author(s)
Marco Klein Heerenbrink
References
Pennycuick, C. J. (2008). Modelling the flying bird. Amsterdam, The Netherlands: Elsevier.
See Also
Examples
## Define a bird:
myBird = Bird(
massTotal = 0.215, # (kg) total body mass
wingSpan = 0.67, # (m) maximum wing span
wingArea = 0.0652, # (m2) maximum wing area
type = "passerine"
)
## define a speed range
speedrange <- seq(5,14,length.out=5)
## compute aerodynamic power for that speed range:
Paero <- computeFlappingPower(myBird,speedrange)
Pchem <- Paero
Pchem$power <- mech2chem(Paero$power,myBird)
print(Pchem[c("speed","power","frequency","strokeplane")])
# speed power frequency strokeplane
# 1 5.00 15.60151 5.948083 46.56887
# 2 7.25 12.44362 5.948083 31.89129
# 3 9.50 12.79900 5.948083 22.51896
# 4 11.75 15.36721 5.948083 16.49120
# 5 14.00 19.82915 5.948083 12.09174
Pmech <- Pchem
Pmech$power <- chem2mech(Pchem$power,myBird)
print(Pmech[c("speed","power","frequency","strokeplane")])
# speed power frequency strokeplane
# 1 5.00 2.789751 5.948083 46.56887
# 2 7.25 2.129466 5.948083 31.89129
# 3 9.50 2.203773 5.948083 22.51896
# 4 11.75 2.740763 5.948083 16.49120
# 5 14.00 3.673714 5.948083 12.09174