Sets HWK08: Problem 3 em Problem List Previous Problem Next Problem ngs (4 points) Air enters...
Air at 10 degree C and 80 kPa enters the diffuser of a jet engine steadily with a velocity of 200 m/s. The inlet area of the diffuser is 0.4 m^2.The air leaves the diffuser with a velocity that is very small compared with the inlet velocity. Determine the mass flow rate of the air and the temperature of the air leaving the diffuser. Air at 100 kPa and 280 K is compressed steadily to 600 kPa and 400 K....
Sets FTC Part I: Problem 9 em 9 Previous Problem Problem List Next Problem ngs Results for this submission ents ards Entered Answer Preview oblems 2.6856 2.6856 The answer above is NOT correct. (1 point) Evaluate the definite integral 3 da 5 2.68560 Type here to search e a
I need question 4 thermodynamics ll 1-v diagram. Problem (4) team enters a turbine operating on SSSF process with mass flow turbine develops a power out put of 100 K temperature is 400 °C, and the velocity is 10 m/s. At the e quality is 0.9, and the velocity is 50 m/s. Determine the rate of heat transfer from the turbine (KW). (10 marks) rate of 4600 kg/hr. The W. At the inlet, the pressure is 6 MPa, the ure...
Problem-2 (200) Air at 30 kPa, 200 K, and 250 m/s enters a turbojet engine in flight. The air mass flow rate is 28 kg/s. The compressor pressure ratio is 13, the turbine inlet temperature is 1460 K, and air exits the nozzle at 30 kPa. The diffuser and nozzle processes are isentropic, the compressor and turbine have isentropic efficiencies of 81% and 88%, respectively, and there is no pressure drop for flow through the combustor. Kinetic energy is negligible...
Problems for Week 9: Problem 4 Previous Problem Problem List Next Problem (2 points) Compute the surface area of revolution of y 4x + 3 about the x-axis over the interval [4,5]. S = Preview My Answers Submit Answers You have attempted this problem 1 time. Your overall recorded score is 0 %. You have unlimited attempts remaining. Email instructor
5-30 Air enters an adiabatic nozzle steadily at 300 kPa, 200°C, and 30 m/s and leaves at 100 kPa and 180 m/s. The inlet area of the nozzle is 80 cm². Determine (a) the mass flow rate through the nozzle, (b) the exit temperature of the air, and (c) the exit area of the nozzle. Answers: (a) 0.5304 kg/s, (b) 184.6°C, (c) 38.7 cm P = 300 kPa T, = 200°C Vi = 30 m/s A = 80 cm AIR...
HW17: Problem 3 Previous Problem Problem List Next Problem (4 points) Find the amount due if $900 is borrowed for 10 months at 16% annual simple interest. Amount = $ Preview My Answers Submit Answers You have attempted this problem 1 time. Your overall recorded score is 0%. You have unlimited attempts remaining.
Assignment1: Problem 4 Previous Problem Problem List Next Problem (3 points) For what value(s) of the constant a is the differential equation dr dr = tela-3)x drž + (a de a linear equation? Preview My Answers Submit Answers You have attempted this problem 0 times. You have unlimited attempts remaining. Email instructor
IMAA MATHEMATICAL ASSOCIATION OF AMERICA rk K webwork /2019s1_math_200_921 / homework2/6 Sets Homework2: Problem 6 Previous Problem Problem List Next Problem gs (1 point) Find the area of the parallelogram defined by the vectors lems -3 Area - Preview My Answers Submit Answers You have attempted this problem 0 times. You have unlimited attempts remaining. Email instructor 10 V Page generated at 05/18/2019 at 01:42pm PDT 1996-2017I theme: math4 I ww version: WeBWork-2.13 pg_version PG-2.13 WeBWork IMAA MATHEMATICAL ASSOCIATION OF...
HW18: Problem 2 Previous Problem Problem List Next Problem (4 points) Find the principal needed to get $700 in 6 years at 4% compounded monthly. Principal = $ 11 Preview My Answers Submit Answers You have attempted this problem 0 times. You have unlimited attempts remaining.