GATE AE · 2017 · AE
Question 42: Special Topics
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Question 42
AEMCQ2 marksNeeds review
The roots obtained by solving longitudinal characteristic equations of motion for a statically stable aircraft are given below:
, where
The undamped short-period longitudinal natural frequency (radians/sec) and damping ratio, in that order, are close toYour answerChoose one option.
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2017AE
GATE AE 2017 · Paper 1
Aerospace Engineering · Original paper archive
- Section
- Aerospace Engineering
- Question type
- Multiple choice (MCQ)
- Marks
- 2 marks
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