General Questions (70)

11. Module 8: Set 1, 60-80, question 17. Two similar answers.
12. Does aircraft maintainance engineering have good scope ? Availability of jobs?
13. Why division by zero is undefined . i think it is infinity
14. I completed my B.E in aeroanutical engineering in 2011. I got married and couldnt continue my studies. now again i want to take up my career in aero field. am totally blank on what to do next. What are the opportunities for higher studies...Can u pl help me to find out the opportunities ..
15. After my diploma in aeronautical engineering. I would like to do piloting so what are the ways to choose a path in piloting
16. Physics, question bank, set3, 6-10, question no 7, i can't understand can you explain
17. Subject:physics question bank, set3, 6-10, question 9, seems to be wrong on nov 11 2015
18. Question bank, set 3, 6-10, question 9, seems to wrong on Nov 10 2015
19. Question bank, set 3, 6-10, question no 7, i can\'t understand can you explain
20. In the the module 15 set 2 , qustion 41-60 question no 13# In a gas turbine engine, turbine section 1#temperature decreases along with pressure and velocity 2#velocity decreases and pressure increases 3#velocity increases and pressure decreases. i think the answer should be re checked because in turbine section all kinds of energies are converted into the mechanical energy like kinetic pressure and heat energy all are converted into mechanically majorly so how could velocity increases in that.. yup in exhaust nozzle velocity increases but how can it be in turbine section..
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