GATE AE · 2025 · AE
Question 48: Basic Fluid Mechanics
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Question 48
AENAT2 marksNeeds review
In a low-speed airplane, a venturimeter with 1.3:1 area ratio is used for airspeed measurement. The airplane’s maximum speed at sea level is 90 m/s. If the density of air at sea level is 1.225 kg/m
, the maximum pressure difference between the inlet and the throat of the venturimeter is
kPa (rounded off to two decimal places).Log in to check the answer
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2025AE
GATE AE 2025 · Paper 1
Aerospace Engineering · Original paper archive
- Section
- Aerospace Engineering
- Question type
- Numerical answer (NAT)
- Marks
- 2 marks
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