GATE AE · 2019 · AE
Question 39: Airfoils and Wings
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Question 39
AENAT2 marksNeeds review
The span-wise distribution of circulation over a finite wing of span
m is
If
m
/s and the free stream density and speed are 1.2 kg/m
and 100 m/s, respectively, the total lift is ______ kN (round off to 2 decimal places).Log in to check the answer
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2019AE
GATE AE 2019 · Paper 1
Aerospace Engineering · Original paper archive
- Section
- Aerospace Engineering
- Question type
- Numerical answer (NAT)
- Marks
- 2 marks
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