subject
Engineering, 14.06.2021 15:20 jaylanmahone223

Se quema n-octano [C8H18(l)] en la cámara de combus- tión de presión constante del motor de un avión con 70 por ciento de exceso de aire, que entra a la cámara de combustión a 600 kPa y 327 °C. Se inyecta combustible líquido a 25 °C, y los productos de combustión salen a 600 kPa y 1 227 °C. Determi- ne la generación de entropía y la destrucción de exergía por unidad de masa de combustible durante este proceso de com- bustión.

ansver
Answers: 1

Other questions on the subject: Engineering

image
Engineering, 03.07.2019 23:20, abbz13
Two technicians are discussing the intake air temperature (iat) sensor. technician a says that the computer uses the iat sensor as a backup to the engine coolant temperature (ect) sensor. technician b says that the powertrain control module (pcm) will subtract the calculated amount of fuel if the air measures hot. who is correct
Answers: 3
image
Engineering, 04.07.2019 18:10, hadellolo8839
Acompressor receives the shaft work to decrease the pressure of the fluid. a)- true b)- false
Answers: 3
image
Engineering, 04.07.2019 18:10, oshawn108
Ahot wire operates at a temperature of 200°c while the air temperature is 20°c. the hot wire element is a tungsten wire of 5 um diameter and 2 mm in length. plot using excel current, heat transfer and heat generated by the wire for air velocity varying from 1-10 m/s in steps of lm/s? matlab the sensor voltage output, resistance, or assume nu 0.989 re033pr13 take air properties at tr (200°c20°c)/2 = 110°c properties of tungsten: c 0.13 kj/kg. k 3 p 19250 kg/m k (thermal conductivity) = 174 w/m. k
Answers: 2
image
Engineering, 04.07.2019 18:10, mamasbug4285
An air compression refrigeration system is to have an air pressure of 100 psia in the brine tank and an allowable air temperature increase of 60°f for standard vapor compression cycle temperatures of 77 f entering the expansion cylinder and 14 f entering the compression cylinder, calculate the coefficient of performance a. 2.5 b 3.3 c. 4.0 d. 5.0
Answers: 3
You know the right answer?
Se quema n-octano [C8H18(l)] en la cámara de combus- tión de presión constante del motor de un avión...

Questions in other subjects:

Konu
Chemistry, 12.11.2020 18:50
Konu
Business, 12.11.2020 18:50