GATE AE · 2019 · AE
Question 19: Atmosphere
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Question 19
AENAT1 markNeeds review
An airplane is in steady level flight with a true air speed of 50 m/s. The ambient air density and ambient pressure at the flight altitude are 0.91 kg/m
and
N/m
, respectively. At sea level, air density is 1.225 kg/m
and ambient pressure is
N/m
. The equivalent or indicated air speed of the airplane is ______ m/s (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
- 1 mark
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