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Recent questions tagged 2013
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The object of providing masked inlet valve in the air passage of compression ignition engines is to
asked
Jan 26, 2018
in
IC Engines
by
chandu
(
215k
points)
ies-objectives-1
2013
ic-engines
carburetion-diesel-injection
0
votes
0
answers
In SI engines for higher thermal efficiency
asked
Jan 26, 2018
in
IC Engines
by
chandu
(
215k
points)
ies-objectives-1
2013
ic-engines
air-standard-cycle
0
votes
0
answers
What is the temperature after isentropic expansion if ratio of specific heats is 1.4?
asked
Jan 26, 2018
in
IC Engines
by
chandu
(
215k
points)
ies-objectives-1
2013
ic-engines
air-standard-cycle
0
votes
0
answers
For a given compression ratio, which of the following ideal cycles have equal thermal efficiency?
asked
Jan 26, 2018
in
IC Engines
by
chandu
(
215k
points)
ies-objectives-1
2013
ic-engines
air-standard-cycle
0
votes
0
answers
What is the water flow rate per hour?
asked
Jan 25, 2018
in
R&AC
by
chandu
(
215k
points)
ies-objectives-1
2013
r&ac
heat-pump&refrigeration-system
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votes
0
answers
Which of the following statements are correct for turbo-prop powered aircrafts?
asked
Jan 17, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
2013
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
Then propulsive efficiency is
asked
Jan 17, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
2013
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
The air fuel ratio at this altitude will be
asked
Jan 17, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
2013
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
Which of the following statements are correct for rockets?
asked
Jan 17, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
2013
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
In an adiabatic flow with friction through a constant area duct, the following phenomenons are predicted:
asked
Jan 17, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
2013
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
Fanno line flow is a flow a constant area duct
asked
Jan 17, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
2013
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
The flow velocity in the convergent section of the nozzle is
asked
Jan 17, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
2013
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
In an isentropic nozzle flow
asked
Jan 17, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
2013
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
Mass flow through the convergent nozzle is maximum when the exit Mach number is
asked
Jan 17, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
2013
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
When a bluff body moves at supersonic speed in still air
asked
Jan 17, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
2013
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
The solid on being heated will only
asked
Jan 17, 2018
in
TD
by
chandu
(
215k
points)
ies-objectives-1
2013
td
pure-substances
0
votes
0
answers
The mass rate of flow through the cycle will be
asked
Jan 17, 2018
in
TD
by
chandu
(
215k
points)
ies-objectives-1
2013
td
pure-substances
0
votes
0
answers
The risk of radioactive hazard is greatest in the turbine with following reactor
asked
Jan 16, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
2013
ppe
nuclear-science
0
votes
0
answers
Calculate power developed in kW/kg of gas per second and exhaust gas temperature
asked
Jan 16, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
2013
ppe
gas-turbine
0
votes
0
answers
The thermal efficiency of a simple open gas turbine plant is improved by regeneration as this
asked
Jan 16, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
2013
ppe
gas-turbine
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