Description Usage Arguments Details Value References See Also
This function creates a list of user-defined morphological description parameters of an input bird. At least three parameters need to be specified: body mass, wing span and wing area. This definition of the bird is then used by the other functions in the package to estimate flight performance.
1 2 | BirdMorphParam(BMass, WSpan, WArea, C_db = 0.2, C_dpro = 0.2,
ADensity = 1.23, grav = 9.8, k = 1.2)
|
BMass |
Body mass of bird in kilograms (kg) |
WSpan |
Wingspan (maximum distance between wingtips) of bird in meters (m) |
WArea |
Wing area (area of fully stretched wings) of bird in square meters (m2) |
C_db |
Body drag coefficient |
C_dpro |
Profile drag coefficient |
ADensity |
Air density |
grav |
Acceleration due to gravity |
k |
induced drag factor |
This function defines the morphological parameters of an input bird and some
other variables for power calculation. At least three bird parameters, body mass (BMass
), wing span (WSpan
) and
wing area (WArea
), need to be specified.
The default value for both body drag and profile drag coeficient: C_db
and C_dpro
is 0.2. A constant air density
of 1.23 kg/m3 is used with acceleration due to gravity, grav
of 9.8 m/s2.
The induced drag factor, k
, is also given as 1.2 as used in the Flight Program (Pennycuick, 2008).
All default arguments can be varied as suitable. If no arguments are defined, the default values will be used.
Morphological parameters of bird and other variables for power calculation.
Pennycuick, C. J. (2008). Modelling the flying bird (Vol. 5). Elsevier.
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