You are given the following information: • • • Our aircraft, type Piper Archer TX, has a wingspan of 10.3 m Di = x px V2 × CDi × S 2 The following diagram is provided: In the first column of the table, type the correct percentage of normal induced drag as a function of the height above ground provided in the second column. Round up to the nearest multiple of 10. Percentage of normal induced drag 100% 80% 60% 40% 20% 20% 40% 60 % 80% 100% Percentage of span above ground % of normal induced drag Di Aircraft height above ground (m) 2.06 11 1.03 4.12
You are given the following information: • • • Our aircraft, type Piper Archer TX, has a wingspan of 10.3 m Di = x px V2 × CDi × S 2 The following diagram is provided: In the first column of the table, type the correct percentage of normal induced drag as a function of the height above ground provided in the second column. Round up to the nearest multiple of 10. Percentage of normal induced drag 100% 80% 60% 40% 20% 20% 40% 60 % 80% 100% Percentage of span above ground % of normal induced drag Di Aircraft height above ground (m) 2.06 11 1.03 4.12
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I am struggling to work this out can you explain this to me how to work this out using the formula.
Transcribed Image Text:You are given the following information:
•
•
•
Our aircraft, type Piper Archer TX, has a
wingspan of 10.3 m
Di = x px V2 × CDi × S
2
The following diagram is provided:
In the first column of the table, type the correct
percentage of normal induced drag as a function of
the height above ground provided in the second
column.
Round up to the nearest multiple of 10.
Percentage of normal induced drag
100%
80%
60%
40%
20%
20% 40% 60 % 80% 100%
Percentage of span above ground
% of normal induced
drag Di
Aircraft height above
ground (m)
2.06
11
1.03
4.12
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