GATE AE · 2020 · AE
Question 45: Static Stability
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Question 45
AENAT2 marksNeeds review
For a general aviation airplane with tail efficiency
, horizontal tail volume ratio
, downwash angle slope
, wing lift curve slope
rad⁻¹, horizontal tail lift curve slope
rad⁻¹, shift in neutral point location as a percentage of mean aerodynamic chord is ______ (round off to two decimal places).Log in to check the answer
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2020AE
GATE AE 2020 · Paper 1
Aerospace Engineering · Original paper archive
- Section
- Aerospace Engineering
- Question type
- Numerical answer (NAT)
- Marks
- 2 marks
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