3 2. Air Normal Maj = 2.5 P1 = 40 kPa T = 30°C shock

Q: ir, at stagnation conditions of 450 K and 250 kPa, flows through a nozzle. At section 1, where the…

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Q: An air tank of volume 1.5 m3 is initially at 800 kPa and20 °C. At t = 0, it begins exhausting…

A: Given data

Q: What would you have to do to reduce this flow angle to zero degrees?

A: Here the reducing flow by zero degree angle attack

Q: Please answer c A supersonic converging-diverging nozzle is near the exit of a turbojet engine. Its…

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Q: A 50 litre tank takes 4 minutes to fill with petrol (density 733 kg/m3 ) through a nozzle of…

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Q: An ideal gas flows adiabatically through a duct. At section1, p1 =140 kPa, T1 = 2608C, and V1 = 75…

A: Since multiple questions are asked and also it is not specified which question to solve, so as per…

Q: Air, at po = 160 lbf/in2 and To = 300 °F, fl ows isentropicallythrough a converging–diverging…

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Q: An airplane flies at a speed of 324 km/hr at an elevation of 3000m (the standard atmospheric…

A: To Find:the pressure at the stagnation point on the nose of the airplane.the pressure difference…

Q: If the exit Mach number in Fig. is 2.2, what is theexit area?(a) 0.10 m2, (b) 0.12 m2, (c) 0.15 m2,…

A: Write the given data.

Q: Compressible laminar fl ow, f≈ 64/Re, may occur in capillarytubes. Consider air, at stagnation…

A: Given data: *The stagnation temperature of the air is T=100°C. *The stagnation pressure of the air…

Q: 1. Air, with stagnation conditions of 800 kPa and 100 °C, ex pands isentropically to a section of a…

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Q: The village shaman is up to no good again. Having calibrated their pulley system, they now have a…

A: (a) Given data: Wind speed: 5 m/s Amount of potion: n = 104 moles Initial temperature: 20°C Final…

Q: A flow with Mach number M1 = 2 and pressure p1 = 1 atm is turned away from itself twice, first…

A: The diagram for first flow with two turns,

Q: The convergent-divergent nozzle in Figure 22 expands and accelerates dry air to supersonic speeds at…

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Q: Air enters a pipe of 1-cm diameter and 1.2-m length at p1 = 220 kPa and T1 = 300 K. If f = 0.025 and…

A: Given data: The area of the flow is

Q: Folsim calculates the aerodynamic forces using the ideal flow model that neglects viscous and…

A: As, low Re i.e. Laminar flow suitable for the models which neglects viscous and compressibility…

Q: Air from a reservoir at 20°C and 500 kPa flows through a duct and forms a normal shock downstream of…

A: Given data:The temperature of the air at the reservoir is .The pressure at the reservoir is The area…

Q: Consi der a shockwave with an angle of ß= 25° that impinges on a wall at point p (as shown in the…

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Q: 02: Air flows isentropically through converging nozzle which has a throat of 7 cm?. The stagnation…

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Q: The total temperature and total pressure (absolute) in the reservoir of a converging-diverging…

A: The test section area, mass flow rate, pressure, temperature, and airspeed. Given: The temperature…