Engineering, 21.04.2020 21:35 shmote12

Flow in a gas turbine combustor is modeled as steady, one-dimensional, frictionless
heating of air in a channel of constant area. For a certain process, the inlet conditions
are 960°F, 225 psia, and M = 0.4. Calculate the maximum possible heat
addition. Find all fluid properties at the outlet section and the reduction in stagnation
pressure. Show the process path on a Ts diagram, indicating ail static and stagnation
state points.

Answers: 1

Show answers

Another question on Engineering

Engineering, 04.07.2019 18:10

Afull journal bearing has a journal diameter of 27 mm, with a unilateral tolerance of -0.028 mm. the bushing bore has a diameter of 27.028 mm and a unilateral tolerance of 0.04 mm. the l/d ratio is 0.5. the load is 1.3 kn and the journal runs at 1200 rev/min. if the average viscosity is 50 mpa-s, find the minimum film thickness, the power loss, and the side flow for the minimum clearance assembly.

Answers: 1

Answer

Engineering, 04.07.2019 18:10

Shafts are machine elements that are used to a) carry axial loads b) direct shear loads c) transmit power d) rotate at constant speed e) none of the above circular and square shafts subjected to the same torque under the same circum behave a) the same way b) almost the same way

Answers: 2

Answer

Engineering, 04.07.2019 18:20

Asimple rankine cycle uses water as the working fluid. the water enters the turbine at 10 mpa and 480c while the condenser operates at 6 kpa. if the turbine has an isentropic efficiency of 80 percent while the pump has an isentropic efficiency of 70 percent determine the thermal efficiency

Answers: 1

Answer

Engineering, 04.07.2019 18:20

Atank with constant volume contains 2.27 kg of a mixture of water phases (liquid-vapor). in the initial state the temperature and the quality are 127 °c and 0.6, respectively. the mixture is heated until the temperature of 160 oc is reached. illustrate the process in a t-v diagram. then, determine (1) the mass of the vapor in kg at the initial state, (2) the final pressure in kpa.

Answers: 3

Answer

You know the right answer?

Flow in a gas turbine combustor is modeled as steady, one-dimensional, frictionless
heating o...

Questions

SAT, 24.10.2021 02:00

Analiza los vicios pragmáticos que existen en las canciones antiguas y de actualidad...