Low speed wind tunnel is explained and the continuity and Bernoulli equations are used to get the flow field relationships between pressure, area of cross section and velocity. The formula for calculating the velocity at the test section is derived. The working principle of the manometer and the types of liquids which can be used in this device are discussed.
#aerospaceengineering #gateaerospaceengineering
#aerodynamics
#windtunnel
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