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3.) Determine the induced drag force developed if a wing of span area 36m^2 and chord of 2.4m has a lift coefficient of 1.2, and the aircraft is traveling at 52kts, and standard sea-level conditions. If total drag force developed is 2000N, what is parasite drag developed? Discuss the difference between parasite drag and induced drag and how it varies with velocity of an aircraft, as reflected on aircraft drag polar curve. Where is V_stall located on the plot?

3.) Determine the induced drag force developed if a wing of span area 36m^2 and chord of 2.4m has a lift coefficient of 1.2, and the aircraft is traveling at 52kts, and standard sea-level conditions. If total drag force developed is 2000N, what is parasite drag developed? Discuss the difference between parasite drag and induced drag and how it varies with velocity of an aircraft, as reflected on aircraft drag polar curve. Where is V_stall located on the plot?

Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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3.) Determine the induced drag force developed if a wing of span area 36m^2 and chord of 2.4m has a lift coefficient of 1.2, and the aircraft is traveling at 52kts, and standard sea-level conditions. If total drag force developed is 2000N, what is parasite drag developed? Discuss the difference between parasite drag and induced drag and how it varies with velocity of an aircraft, as reflected on aircraft drag polar curve. Where is V_stall located on the plot?
Transcribed Image Text:3.) Determine the induced drag force developed if a wing of span area 36m^2 and chord of 2.4m has a lift coefficient of 1.2, and the aircraft is traveling at 52kts, and standard sea-level conditions. If total drag force developed is 2000N, what is parasite drag developed? Discuss the difference between parasite drag and induced drag and how it varies with velocity of an aircraft, as reflected on aircraft drag polar curve. Where is V_stall located on the plot?
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