AEROLAB MODULE 4 Flashcards
After a tunnel is designed, the next
step is to decide its _____________ and, of course, to
modify that which is unsatisfactory
for the intended purposes.
flow
characteristics
Wind Tunnel instruments that uses pressure
Manometer, Barometer, Transducers
Pressure is balanced by the
weight of the liquid
column.
Manometer
Used to measure
atmospheric pressure.
Barometer
Converts pressure to an
analog electrical signal.
Transducers
Why do we calibrate?
To ensure the accuracy
To control errors
Help assure precise
measurements
While doing the
Calibration, some
properties are to be
measured:
Air Speed
Flow Angularity
Turbulence Measurement
Setting the speed of the
wind tunnel is done when
the is _______ the
test section.
no model inside
This can be put
inside the test section to
determine the airspeed.
Pitot Tube
The tunnel speed is usually determined by
__________________ in
the settling chamber in front of the
contraction tube, as station L indicates,
and a static pressure in front of the test
section as station S indicates.
measuring either static or total pressure
The ___________ is usually measured
throughout selected regions of the test
section by means of a pitot-static tube.
The __________ is calculated from a
barometric pressure measurement, and a
test-section temperature determination
along with the equation of state.
dynamic pressure ; density
The variation of q in the working range of
the jet should be less than _____ from the
mean, which corresponds to a _____
variation in velocity.
0.50% ; 0.25%
_________ may be added in the largest section
of the tunnel with spatial mesh densities
varied so that they are more dense in the
sections that correspond to high-velocity
regions in the jet.
screens
The flow has to be uniform across the cross section with all stream lines _______ to the tunnel axis when the test section is empty.
parallel
The flow direction can be calculated by using _____________________.
Sphere type and Claw type yaw meter