How to practice concept:induced-drag

Attempt a question, record the concept and assumptions, then check the available answer. Rework mistakes after revising the relevant concepts. Topic tags can overlap; review the question context.

Questions 1–6 of 6. Imported answers require independent review unless marked reviewed.

Topic practice 6 questionsPage 1 of 1

Question 20

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AEMCQ1 markNeeds review
The fundamental purpose of the Kutta condition in the thin airfoil theory is ________.
Your answerChoose one option.

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Question 35

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AENAT1 markNeeds review
An elliptic wing has a span of 6 m and a planform area of 6 m

. When generating a lift coefficient of 0.6, the induced drag it incurs is ________

(rounded off to 1 decimal place).

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Question 48

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AEMSQ2 marksNeeds review
What is/are the use(s) of the single horseshoe vortex model of finite wing aerodynamic theory?
Your answerSelect all correct options. You can choose more than one.

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Question 36

Open question
AEMCQ2 marksNeeds review
A lifting surface has a spanwise circulation distribution of

(where

) over its span

, and

is the spanwise coordinate. Furthermore, the downwash varies along the span as

, where

is the free stream velocity. Which one of the following options represents total lift (

) and induced drag (

)?
Your answerChoose one option.

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Question 64

Open question
AENAT2 marksNeeds review
An airplane of mass 1000 kg is in a steady level flight with a speed of 50 m/s. The wing has an elliptic planform with a span of 20 m and planform area 31.4 m

. Assuming the density of air at the altitude to be 1 kg/m

and acceleration due to gravity to be 10 m/s

, the induced drag on the wing is ________ N (rounded off to 1 decimal place).

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Question 41

Open question
AENAT2 marksNeeds review
A finite wing of elliptic planform with aspect ratio 10, whose section is a symmetric airfoil, is placed in a uniform flow at 5 degrees angle of attack. The induced drag coefficient for the wing is ______ (round off to three decimal places).

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