The mass flow rate of air through an aircraft engine is $10 \mathrm{~kg} / \mathrm{s}$. The compressor outlet temperature is $400 \mathrm{~K}$ and the turbine inlet temperature is $1800 \mathrm{~K}$. The heating value of the fuel is $42 \mathrm{MJ} / \mathrm{kg}$ and the specific heat at constant pressure is $1 \mathrm{~kJ} / \mathrm{kg}-\mathrm{K}$. The mass flow rate of the fuel in $\mathrm{kg} / \mathrm{s}$ is approximately_____________

Question ID - 156014 :-

The mass flow rate of air through an aircraft engine is $10 \mathrm{~kg} / \mathrm{s}$. The compressor outlet temperature is $400 \mathrm{~K}$ and the turbine inlet temperature is $1800 \mathrm{~K}$. The heating value of the fuel is $42 \mathrm{MJ} / \mathrm{kg}$ and the specific heat at constant pressure is $1 \mathrm{~kJ} / \mathrm{kg}-\mathrm{K}$. The mass flow rate of the fuel in $\mathrm{kg} / \mathrm{s}$ is approximately_____________

We hope we have given the updated helpful answer / content for your query in an easily accessible format to help you in preparing adequately.
We do offer free support materials, 11th maths guide 11th maths guide12th maths guide10th maths guide, also for all the classes books and guide to all the students who sign up for SaraNextGen. Apart from traditional textbook queries, we've got conjointly provided further high order level thinking issues, that are seemingly to be expected in boards and competitive exams. It includes conceptual queries, MCQs, Long and short answer type queries, etc. These Questions are designed to learn each student and academics by providing chapter-wise further issues focusing totally on testing conceptual information with applications.
Here, we've got provided a number of the necessary ways in which within which the solutions of all the Questions will profit students of class 1 to 12. If you have any queries,
drop a message to us and we will get back to you at the earliest.