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Part A The Mach number of the air flow out the nozzle at B is M-04....
Part B Review The large tank contains air at an absolute pressure of 64 psi and temperature of 70 F The nozzle has a th...
Part B Review The large tank contains air at an absolute pressure of 64 psi and temperature of 70 F The nozzle has a throat diameter of 1 in. and an exit diameter of 1.75 in. (Figure 1) Determine the absolute pressure within the connected pipe, when the nozzle chokes and maintains isentropic supersonic flow within the divergent section of the nozzle. Express your answer to three significant figures and include the appropriate units P- psi Submit Incorrect; Try Again...
< Fluids-HW13A Problem 13.34 A converging nozzle having an exit diameter of 30 mm is connected...
< Fluids-HW13A Problem 13.34 A converging nozzle having an exit diameter of 30 mm is connected to the large tank (Figure 1). The absolute pressure outside the tank is 102 kPa. Part A If the temperature of the air in the tank is 20°C and the absolute pressure is 480 kPa, determine the mass flow from the tank. Express your answer using three significant figures. 180 AED U vec * O ? m = 0.1289 kg/s Submit Previous Answers Request...
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 o...
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...
5 kg/s through an insulated circular duct such that the (gauge) pressure immediately downstream of a blower is 10 kPa....
5 kg/s through an insulated circular duct such that the (gauge) pressure immediately downstream of a blower is 10 kPa. You may neglect the impact of elevation change in your analysis. Air flows at 0 Part A If the pressure at a downstream location within the duct is measured as 8 kPa, estimate the change in the temperature of the air that would be expected between upstream and downstream locations three significant figures. Express your answer VAE uT vec AT...
Air (use the PG model) enters the compressor of an ideal air standard Brayton cycle at...
Air (use the PG model) enters the compressor of an ideal air standard Brayton cycle at 100 kPa and 305 K with a volumetric flow rate of 5 m/s. The compressor pressure ratio is 12. The turbine inlet temperature is 1000 K. Part A Determine the thermal efficiency (17th, Brayton) Express your answer to three significant figures. V AED 11 vec Submit Request Answer Part B Determine the net power output (Wet). Express your answer to six significant figures and...
A nozzle is designed to deliver a supersonic air flow, R = 287 J/Kg/K, of Mach...
A nozzle is designed to deliver a supersonic air flow, R = 287 J/Kg/K, of Mach M = 2.19 The reservoir has a pressure of p0 = 648kPa and T0= 300K. The nozzle exit has an area of 0.233 m^2. The nozzle flow exits into an environment that is kept at constant pressure pb which matches the exit pressure of the nozzle. As long as there are no shock waves appearing in – or outside the nozzle, the complete flow...
Problem 5.61 %) Item 2 Part A (Figure 1 If d-1.5 m, and 30P, determine the...
Problem 5.61 %) Item 2 Part A (Figure 1 If d-1.5 m, and 30P, determine the normal reaction at the smooth support A if P 450 N. Neglect the weight of the bar Express your answer using three significant figures and include the appropriate units. NAValue Units Figure 1 of 1 Submit Part B Determine the normal reaction at the smooth support B Express your answer using three significant figures and include the appropriate units. NValue Units Submit Reguest Answer...
Problem 16.104 Part A Determine the acceleration of the top of the ladder, B At a...
Problem 16.104 Part A Determine the acceleration of the top of the ladder, B At a given instant the bottom A of the ladder has an acceleration aA 4.6 ft/s and velocity vA 6.0 ft/s, both acting to the left. (Figure 1) Express your answer to three significant figures and include the appropriate units. aValue Units Submit An Figure 1of1 〉 Part B Determine the ladder's angular acceleration at this same instant Express your answer to three significant figures and...
if you sure then solve. will be rate Air flows at 0.05 kg/s through n insulated circular duct such that the (gauge)...
if you sure then solve. will be rate
Air flows at 0.05 kg/s through n insulated circular duct such that the (gauge) pressure immediately downstream of a blower is 10 kPa You may neglect the impact of elevation change in your analysis. Part A the air that would be expected between upstream and downstream locations. If the pressure at a downstream location within the duct is measured as 8 kPa, estimate the change the temperature Express your answer to three...
Part A The resultant of the three forces acting on the bracket is FR-(-330 k} lb...
Part A The resultant of the three forces acting on the bracket is FR-(-330 k} lb Note that F3 lies in the z-y plane Figure 1) Specify the magnitude of F Express your answer to three significant figures and include the appropriate units. FValue Units Figure く 1of1 Submit Request Answer Part B Fs400 Ib Yi Specify the coordinate direction angle a of F Express your answer using three significant figures. 30 F2 200 lb Bi vec ▼ Part C...
Part B Review The large tank contains air at an absolute pressure of 64 psi and temperature of 70 F The nozzle has a throat diameter of 1 in. and an exit diameter of 1.75 in. (Figure 1) Determine the absolute pressure within the connected pipe, when the nozzle chokes and maintains isentropic supersonic flow within the divergent section of the nozzle. Express your answer to three significant figures and include the appropriate units P- psi Submit Incorrect; Try Again...
< Fluids-HW13A Problem 13.34 A converging nozzle having an exit diameter of 30 mm is connected to the large tank (Figure 1). The absolute pressure outside the tank is 102 kPa. Part A If the temperature of the air in the tank is 20°C and the absolute pressure is 480 kPa, determine the mass flow from the tank. Express your answer using three significant figures. 180 AED U vec * O ? m = 0.1289 kg/s Submit Previous Answers Request...
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...
5 kg/s through an insulated circular duct such that the (gauge) pressure immediately downstream of a blower is 10 kPa. You may neglect the impact of elevation change in your analysis. Air flows at 0 Part A If the pressure at a downstream location within the duct is measured as 8 kPa, estimate the change in the temperature of the air that would be expected between upstream and downstream locations three significant figures. Express your answer VAE uT vec AT...
Air (use the PG model) enters the compressor of an ideal air standard Brayton cycle at 100 kPa and 305 K with a volumetric flow rate of 5 m/s. The compressor pressure ratio is 12. The turbine inlet temperature is 1000 K. Part A Determine the thermal efficiency (17th, Brayton) Express your answer to three significant figures. V AED 11 vec Submit Request Answer Part B Determine the net power output (Wet). Express your answer to six significant figures and...
Problem 5.61 %) Item 2 Part A (Figure 1 If d-1.5 m, and 30P, determine the normal reaction at the smooth support A if P 450 N. Neglect the weight of the bar Express your answer using three significant figures and include the appropriate units. NAValue Units Figure 1 of 1 Submit Part B Determine the normal reaction at the smooth support B Express your answer using three significant figures and include the appropriate units. NValue Units Submit Reguest Answer...
Problem 16.104 Part A Determine the acceleration of the top of the ladder, B At a given instant the bottom A of the ladder has an acceleration aA 4.6 ft/s and velocity vA 6.0 ft/s, both acting to the left. (Figure 1) Express your answer to three significant figures and include the appropriate units. aValue Units Submit An Figure 1of1 〉 Part B Determine the ladder's angular acceleration at this same instant Express your answer to three significant figures and...
if you sure then solve. will be rate
Air flows at 0.05 kg/s through n insulated circular duct such that the (gauge) pressure immediately downstream of a blower is 10 kPa You may neglect the impact of elevation change in your analysis. Part A the air that would be expected between upstream and downstream locations. If the pressure at a downstream location within the duct is measured as 8 kPa, estimate the change the temperature Express your answer to three...
Part A The resultant of the three forces acting on the bracket is FR-(-330 k} lb Note that F3 lies in the z-y plane Figure 1) Specify the magnitude of F Express your answer to three significant figures and include the appropriate units. FValue Units Figure く 1of1 Submit Request Answer Part B Fs400 Ib Yi Specify the coordinate direction angle a of F Express your answer using three significant figures. 30 F2 200 lb Bi vec ▼ Part C...
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