Consider the nozzle given below. The nozzle exit has an area 0.0011 m^2 and a pressure of 0 kPa (gauge). Given the mass flow and cross sectional area of the nozzle entrance, what is the pressure at the nozzle entrance (P1) ? Give the answer in kPa gauge, but do not enter the units in the answer box. The fluid is water with a density of 1000 kg/m^3. Ignore work and friction. The external force is still unknown.
mass flow = 37 kg/s
Nozzle entrance = 0.0061 m^2
Pressure at nozzle entrance (P1) = ?
Consider the nozzle given below. The nozzle exit has an area 0.0011 m^2 and a pressure...
Question 1.4 A convergent-divergent nozzle is designed to operate with isentropic flow with an exit Mach number, Me. The flowin the nozzle is supplied from a reservoir of air with a static pressure ofPr and a static temperature of Tr and the nozzle has a throat area, AT, as specified in the table below Value Unit Design Data Exit Mach number (ME) 0.55 Area of throat (AT) 600 kPa Reservoir static pressure (PR) 380 WAT Reservoir static temperature (TR) kPa...
PROBLEM 1 (50 points) Pa= 100 kPa D=0.1 m Po=500 kPa To-300 K Convergent nozzle alone Nozzle Exit Pa 100 kPa f- 0.005 D= 0.1 m Po=500 kPa To-300 K Convergent nozzle + pipe L= 10 m Nozzle Exit Pipe Exit A convergent nozzle of diameter D = 0.1 m is connected to a reservoir with pressure po=500 kPa The convergent nozzle supplies flow to a pipe of equal diameter with length L = 10 m and friction factor f...
Water steam is running through the nozzle. Inlet pressure is P1=25 bars; T1=300C; V1=90m/s; A1=0.2m2. The exit parameters are: P2=11bars; T2=210C. The mass flow rate is m=2 kg/s. Determine: Exit velocity V2=?; Inlet and outlet diameters D1 and D2
Fundamentals-of-Compressible-Fluid-Dynamics Balachandran CHAPTER 4 6. A conical diffuser of 15 cm has an area ratio of 4. If the pressure, temperature and velocity at the inlet section are 0.69 bar, 340 K and 180 m/s, estimate the exit pressure and exit velocity. What will be the change in impulse function. [Ans. p2 = 0.8074 bar; V2 = 45 m/s; F2 - F1 = 4167.5 N] 7. The Mach number at inlet and exit of a supersonic diffuser are 3 and...
Question 2 (30 marks) (a) A fluid flowing into a nozzle with specific enthalpy of 2980 kJ/kg and the velocity is 80 m/s. At the exit of the nozzle, the specific enthalpy of the fluid drops to 2670 kJ/kg. The nozzle orientation is horizontal and the heat loss is negligible. Given that the nozzle inlet area is 0.25 m2 and the specific volume of the fluid is 0.2 m2/kg, calculate the velocity of the fluid at exit, the mass flow...
A converging-diverging nozzle has a throat area of 1 cm2 and an exit area of 4 cm2. The inlet stagnation conditions are Po 500 kPa and To 300 K. The nozzle discharges to an infinite surroundings at Po. The flowing medium is air as a perfect gas with k-1.4 Answer the following: i What are the two isentropic flow solutions for this nozzle with M 1 at the throat? What are the Mach number, P, Po and T, To at...
1. (15 pts) A converging-diverging nozzle has an area ratio of 2, i.e., the exit (or duct) area is 2 times the throat area, which is 80 cm2. The nozzle is supplied from a tank containing air (y 1.4 and R 287 J/kg K) at 100 kPa and 300K. For both cases shown in Fig. , find the maximum mass flow possible through the nozzle and the range of back pressures over which the mass flow can be attained. For...
1. (15 pts) A converging-diverging nozzle has an area ratio of 2, i.e., the exit (or duct) area is 2 times the throat area, which is 80 cm2. The nozzle is supplied from a tank containing air (y 1.4 and R 287 J/kg K) at 100 kPa and 300K. For both cases shown in Fig. , find the maximum mass flow possible through the nozzle and the range of back pressures over which the mass flow can be attained. For...
4-1-30 [WX] An adiabatic steam nozzle operates steadily under the following conditions. Inlet: superheated vapor, p1 = 1 MPa, T1 = 300°C, A1 78.54 cm2; Exit: saturated vapor, p2 = 100 kPa. Determine (a) the exit velocity (V2) in m/s, (b) the rate of entropy Solution] [Discuss] generation (Šgen) in kW/K. The mass flow rate (m is 1 kg/s.
9. A constant-area duct connected to a C-D nozzle with 1,687. The nozzle is fed by a large compress-air tank with pressure of 700 kPa and temperature of 540 K. The flow is shockless everywhere and is supersonic at the nozzle exit. Between section 1 and 2, heat added into the duct at a rate of 100.4 kJ/(kg of air). Assuming frictionless flow and ideal gas. Find these properties at section 2: M2. P2.T2 and Poz. 1, nozzle exit Po...