The turbine of an aircraft uses 100kg/s of fuel to perform a flight speed and generates gases at its exit. The air inlet speed of this turbine is 100 m/s. In this system, we know that rhoAR = 1.2kg/m^3 , rhoGASES = 0.8kg/m^3 and that the turbine has its dimensions according to the figure below. From the information given, what is the velocity of the gases generated at the exit?
The turbine of an aircraft uses 100kg/s of fuel to perform a flight speed and generates gases at its exit. The air inlet speed of this turbine is 100 m/s. In this system, we know that rhoAR = 1.2kg/m^3 , rhoGASES = 0.8kg/m^3 and that the turbine has its dimensions according to the figure below. From the information given, what is the velocity of the gases generated at the exit?
Introduction to Chemical Engineering Thermodynamics
8th Edition
ISBN:9781259696527
Author:J.M. Smith Termodinamica en ingenieria quimica, Hendrick C Van Ness, Michael Abbott, Mark Swihart
Publisher:J.M. Smith Termodinamica en ingenieria quimica, Hendrick C Van Ness, Michael Abbott, Mark Swihart
Chapter1: Introduction
Section: Chapter Questions
Problem 1.1P
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The turbine of an aircraft uses 100kg/s of fuel to perform a flight speed and generates gases at its exit. The air inlet speed of this turbine is 100 m/s. In this system, we know that rhoAR = 1.2kg/m^3 , rhoGASES = 0.8kg/m^3 and that the turbine has its dimensions according to the figure below. From the information given, what is the velocity of the gases generated at the exit?
Transcribed Image Text:COMBUSTÍVEL
ENTRADA DE AR
SAÍDA DOS GASES
A1=0,5m^2
A2=0,3m^2
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