What is the static pressure at this location

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Reference no: EM131248275

A single stream tube is selected to characterize the air flow past the wing of an aircraft in flight at an altitude of 20,000 ft at an airspeed of 275 ft/s. The free stream crosssectional area of the stream tube is 0.07 ft 2 .

(a) What is the air flow speed in the stream tube at a location near the wing where the cross-sectional area of the stream tube is 0.05 ft 2? What is the static pressure at this location?

(b) What is the air flow speed in the stream tube at a location near the wing where the cross-sectional area of the stream tube is 0.04 ft 2? What is the static pressure at this location?

Reference no: EM131248275

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