Aerospace Engineering > GATE 2009 > Combustor Design
The division of feed air to an aircraft gas-turbine combustor into primary and secondary streams serves
which of the following purposes ?
P. a flammable mixture can be formed
Q. cooling of combustor liner and flame tube can be accomplished
R. specific fuel consumption can be reduced
which of the following purposes ?
P. a flammable mixture can be formed
Q. cooling of combustor liner and flame tube can be accomplished
R. specific fuel consumption can be reduced
Correct : c
Similar Questions
If → denotes increasing order of intensity, then the meaning of the words dry → arid → parched is analogous to diet → fast → ______. Which one of the given opt...
If two positive non-zero real variables x and y are such that (x+y) is proportional to x/y, then x+y:
Consider the following sample of numbers: 9, 18, 11, 14, 15, 17, 10, 69, 11, 13. The median of the sample is
Total Unique Visitors
Loading......