Alpha-Log
–
User manual
LSI LASTEM SRL
INSTUM_03388
Page 71 / 116
Fig. 33
–
ICAO equations 28 and 29 reference
Fig. 34 - Example of calculated measurement configuration of type "QNH - ICAO"
4.2.3.8
Wind component in aeronautics
Alpha-Log calculates the transverse wind component, in the tail and in the bow depending on the angle of
the landing strip relative to the North.
The formulas used are:
𝐶𝑊 = 𝐴𝐵𝑆(𝑉 × 𝑠𝑖𝑛(𝐷 − 𝐷
𝑟
))
𝐻𝑊 = 𝑉 × 𝑐𝑜𝑠(𝐷 − 𝐷
𝑟
)
𝑇𝑊 = 𝑉 × 𝑐𝑜𝑠(180 + 𝐷−𝐷
𝑟
)
where:
•
CW
= Cross Wind
•
HW
= Head Wind
•
TW
= Tail Wind
•
V
= Wind speed measured near the airstrip
•
D = Wind direction measured near the airstrip
•
D
r
= Orientation direction of the landing strip with direction of travel relative to the indicated angle
Consider the following aspects:
•
The direction measured by the anemometer is conventionally referred to the
origin
of the wind,
while the direction of the aircraft is its
destination
.
•
If
Head Wind
is greater than zero, it indicates presence of the wind component at the bow of the
aircraft.
•
If
Tail Wind
is greater than zero, it indicates the presence of the wind component at the tail of the
aircraft.
•
If
Cross Wind
is greater than zero, it indicates the presence of the transverse wind component on the
aircraft.
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