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Recent questions in IES Conventional-1
0
votes
0
answers
Calculate the stochiometric air fuel ratio for complete combustion
asked
Nov 3, 2017
in
Thermal
by
chandu
(
215k
points)
ies-conventional-1
2014
thermal
fuels-combustion
0
votes
0
answers
Express the quantity of gas contained in the cylinder in moles Treat LPG as Butane
asked
Nov 3, 2017
in
Thermal
by
chandu
(
215k
points)
ies-conventional-1
2013
thermal
fuels-combustion
0
votes
0
answers
Write the resulting chemical reaction and find the equivalence ratio.
asked
Nov 3, 2017
in
Thermal
by
chandu
(
215k
points)
ies-conventional-1
2010
thermal
fuels-combustion
0
votes
0
answers
calculate the mass of air supplied per kg of fuel and
asked
Nov 3, 2017
in
Thermal
by
chandu
(
215k
points)
ies-conventional-1
2009
thermal
fuels-combustion
0
votes
0
answers
How correction for cooling is obtained in this method?
asked
Nov 3, 2017
in
Thermal
by
chandu
(
215k
points)
ies-conventional-1
1999
thermal
fuels-combustion
0
votes
0
answers
Determine (i) the air-fuel ratio on mass basis. (ii) the percent of carbon and hydrogen in the fuel
asked
Nov 3, 2017
in
Thermal
by
chandu
(
215k
points)
ies-conventional-1
1998
thermal
fuels-combustion
0
votes
0
answers
Determine the air fuel ratio on a mass basis and the dew point temperature of the products
asked
Nov 3, 2017
in
Thermal
by
chandu
(
215k
points)
ies-conventional-1
1994
thermal
fuels-combustion
0
votes
0
answers
Find the mass of air required per kg of fuel for complete combustion
asked
Nov 3, 2017
in
Thermal
by
chandu
(
215k
points)
ies-conventional-1
1987
thermal
fuels-combustion
0
votes
0
answers
Explain how the cooling correction is made in the method.
asked
Nov 3, 2017
in
Thermal
by
chandu
(
215k
points)
ies-conventional-1
1987
thermal
fuels-combustion
0
votes
0
answers
Determine (i) the air-fuel ratio, (ii) the percentage of excess air,
asked
Nov 3, 2017
in
Thermal
by
chandu
(
215k
points)
ies-conventional-1
1986
thermal
fuels-combustion
0
votes
0
answers
Describe with the help of a neat sketch the construction and working of an Orsat apparatus
asked
Nov 2, 2017
in
Thermal
by
chandu
(
215k
points)
ies-conventional-1
1986
thermal
fuels-combustion
0
votes
0
answers
Determine the quantity of carbon remaining un burnt in each kg. of the fuel fired in the furnace.
asked
Nov 2, 2017
in
Thermal
by
chandu
(
215k
points)
ies-conventional-1
1983
thermal
fuels-combustion
0
votes
0
answers
Describe with the help of a neat sketch the working of an Orsat apparatus for flue gas analysis.
asked
Nov 2, 2017
in
Thermal
by
chandu
(
215k
points)
ies-conventional-1
1982
thermal
fuels-combustion
0
votes
0
answers
Determine at what air-fuel ratio the engine would be working when it is using iso-octane and ethanol respectively.
asked
Nov 2, 2017
in
Thermal
by
chandu
(
215k
points)
ies-conventional-1
1980
thermal
fuels&combustions
0
votes
0
answers
Determine (i) the velocity at the nozzle exit, and (ii) the pressures & temperatures at each state.
asked
Nov 2, 2017
in
Thermal
by
chandu
(
215k
points)
ies-conventional-1
2006
thermal
jet-propulsion&rocket
0
votes
0
answers
Determine (i) the air-fuel ratio (ii) the specific thrust and (iii) the propulsive efficiency.
asked
Nov 2, 2017
in
Thermal
by
chandu
(
215k
points)
ies-conventional-1
1998
thermal
jet-propulsion&rocket
0
votes
0
answers
Describe with a neat sketch the working of a turbojet engine.
asked
Nov 2, 2017
in
Thermal
by
chandu
(
215k
points)
ies-conventional-1
1996
2010
thermal
jet-propulsion&rocket
0
votes
0
answers
Write a short note on the following (a) Liquid and Solid propellant rockets
asked
Nov 2, 2017
in
Thermal
by
chandu
(
215k
points)
ies-conventional-1
1981
thermal
jet-propulsion&rocket
0
votes
0
answers
What are the distinguishing features of a turbojet and a rocket engine ?
asked
Nov 2, 2017
in
Thermal
by
chandu
(
215k
points)
ies-conventional-1
1979
thermal
jet-propulsion&rocket
engine
0
votes
0
answers
Determine the thermal efficiency of the plant. Assume addition of heat at constant pressure.
asked
Nov 2, 2017
in
Thermal
by
chandu
(
215k
points)
ies-conventional-1
2015
thermal
gas-turbine
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