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Recent questions in IES Objectives-1
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Rayleight line flow is a flow in a constant area duct
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Jan 16, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
1997
ppe
jet-propulsion&compressible-flow
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Fanno line flow is a flow in a constant area duct
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Jan 16, 2018
in
PPE
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chandu
(
215k
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ies-objectives-1
1997
ppe
jet-propulsion&compressible-flow
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Consider the following statements about a rocket engine:
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Jan 16, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
1997
ppe
jet-propulsion&compressible-flow
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For oblique shock, the downstream mach number
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Jan 16, 2018
in
PPE
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chandu
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215k
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ies-objectives-1
1997
ppe
jet-propulsion&compressible-flow
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Across the normal shock, the fluid properties change in such a manner that the
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Jan 16, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
1996
ppe
jet-propulsion&compressible-flow
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0
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Only rocket engines can be propelled to space because
asked
Jan 16, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
1996
ppe
jet-propulsion&compressible-flow
0
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0
answers
Consider the following statements relating to rocket engines:
asked
Jan 16, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
1996
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
In a turbo- jet engine, subsequent to heat addition to compressed air, to get the power output
asked
Jan 16, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
1996
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
In a turbo- jet engine, subsequent to heat addition to compressed air, to get the power output
asked
Jan 16, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
1996
ppe
jet-propulsion&compressible-flow
0
votes
0
answers
In open cycle turbo- jet engines used in
asked
Jan 16, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
1996
ppe
jet-propulsion&compressible-flow
0
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0
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In the subsonic range the propulsive efficiency of a rocket less than
asked
Jan 16, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
1995
ppe
jet-propulsion&compressible-flow
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0
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The propulsive efficiency of the units is
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Jan 16, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
1998
ppe
jet-propulsion&compressible-flow
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0
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In a turbo- jet engine, thrust may be increased by
asked
Jan 16, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
1998
ppe
jet-propulsion&compressible-flow
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0
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The thrust of rocket engine depends upon
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Jan 16, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
1998
ppe
jet-propulsion&compressible-flow
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0
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Which one of the following is the correct sequency of the position of the given components in a Turbo- prop?
asked
Jan 16, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
1998
ppe
jet-propulsion&compressible-flow
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votes
0
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A nuclear unit becoming critical means:
asked
Jan 16, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
2006
ppe
nuclear-science
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0
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What is the function of heavy water in a nuclear reactor?
asked
Jan 16, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
2006
ppe
nuclear-science
0
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0
answers
A nuclear fission is initiated when the critical energy as compared to neutron binding energy atoms is
asked
Jan 16, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
2006
ppe
nuclear-science
0
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0
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Uranium 238 is represented as
asked
Jan 16, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
2007
ppe
nuclear-science
0
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0
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A nuclear reactor is said to be critical when the neutron population in the reactor core is
asked
Jan 16, 2018
in
PPE
by
chandu
(
215k
points)
ies-objectives-1
2008
ppe
nuclear-science
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