GATE AE · 2020 · AE
Question 17: Flight Vehicle Structures
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Question 17
AEMCQ1 markNeeds review
The positive high angle-of-attack condition is obtained in a steady pull-out maneuver at the largest permissible angle-of-attack of the wing. Under this condition, at which of the following regions of the wing does the maximum tension occur?
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2020AE
GATE AE 2020 · Paper 1
Aerospace Engineering · Original paper archive
- Section
- Aerospace Engineering
- Question type
- Multiple choice (MCQ)
- Marks
- 1 mark
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